WO2019140617A1 - 电池控制方法、电池控制***、无人机及电池 - Google Patents

电池控制方法、电池控制***、无人机及电池 Download PDF

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Publication number
WO2019140617A1
WO2019140617A1 PCT/CN2018/073326 CN2018073326W WO2019140617A1 WO 2019140617 A1 WO2019140617 A1 WO 2019140617A1 CN 2018073326 W CN2018073326 W CN 2018073326W WO 2019140617 A1 WO2019140617 A1 WO 2019140617A1
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WIPO (PCT)
Prior art keywords
battery
processor
drone
power supply
supply circuit
Prior art date
Application number
PCT/CN2018/073326
Other languages
English (en)
French (fr)
Inventor
张彩辉
Original Assignee
深圳市大疆创新科技有限公司
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Filing date
Publication date
Application filed by 深圳市大疆创新科技有限公司 filed Critical 深圳市大疆创新科技有限公司
Priority to PCT/CN2018/073326 priority Critical patent/WO2019140617A1/zh
Priority to CN201880031306.XA priority patent/CN110622383B/zh
Publication of WO2019140617A1 publication Critical patent/WO2019140617A1/zh
Priority to US16/927,566 priority patent/US20200338989A1/en

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    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/0029—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries with safety or protection devices or circuits
    • H02J7/00306—Overdischarge protection
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/0047—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries with monitoring or indicating devices or circuits
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L3/00—Electric devices on electrically-propelled vehicles for safety purposes; Monitoring operating variables, e.g. speed, deceleration or energy consumption
    • B60L3/0023—Detecting, eliminating, remedying or compensating for drive train abnormalities, e.g. failures within the drive train
    • B60L3/0046—Detecting, eliminating, remedying or compensating for drive train abnormalities, e.g. failures within the drive train relating to electric energy storage systems, e.g. batteries or capacitors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L3/00—Electric devices on electrically-propelled vehicles for safety purposes; Monitoring operating variables, e.g. speed, deceleration or energy consumption
    • B60L3/0023—Detecting, eliminating, remedying or compensating for drive train abnormalities, e.g. failures within the drive train
    • B60L3/0061—Detecting, eliminating, remedying or compensating for drive train abnormalities, e.g. failures within the drive train relating to electrical machines
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L3/00—Electric devices on electrically-propelled vehicles for safety purposes; Monitoring operating variables, e.g. speed, deceleration or energy consumption
    • B60L3/0023—Detecting, eliminating, remedying or compensating for drive train abnormalities, e.g. failures within the drive train
    • B60L3/0084—Detecting, eliminating, remedying or compensating for drive train abnormalities, e.g. failures within the drive train relating to control modules
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L50/00—Electric propulsion with power supplied within the vehicle
    • B60L50/50—Electric propulsion with power supplied within the vehicle using propulsion power supplied by batteries or fuel cells
    • B60L50/60—Electric propulsion with power supplied within the vehicle using propulsion power supplied by batteries or fuel cells using power supplied by batteries
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L58/00—Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles
    • B60L58/10—Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles for monitoring or controlling batteries
    • B60L58/12—Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles for monitoring or controlling batteries responding to state of charge [SoC]
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/30—Supply or distribution of electrical power
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/0029—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries with safety or protection devices or circuits
    • H02J7/0031—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries with safety or protection devices or circuits using battery or load disconnect circuits
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/0029—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries with safety or protection devices or circuits
    • H02J7/0031—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries with safety or protection devices or circuits using battery or load disconnect circuits
    • H02J7/0032—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries with safety or protection devices or circuits using battery or load disconnect circuits disconnection of loads if battery is not under charge, e.g. in vehicle if engine is not running
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2200/00—Type of vehicles
    • B60L2200/10—Air crafts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2240/00—Control parameters of input or output; Target parameters
    • B60L2240/40—Drive Train control parameters
    • B60L2240/54—Drive Train control parameters related to batteries
    • B60L2240/545—Temperature
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2240/00—Control parameters of input or output; Target parameters
    • B60L2240/40—Drive Train control parameters
    • B60L2240/54—Drive Train control parameters related to batteries
    • B60L2240/547—Voltage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2240/00—Control parameters of input or output; Target parameters
    • B60L2240/40—Drive Train control parameters
    • B60L2240/54—Drive Train control parameters related to batteries
    • B60L2240/549—Current
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2260/00—Operating Modes
    • B60L2260/20—Drive modes; Transition between modes
    • B60L2260/32—Auto pilot mode
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J2310/00—The network for supplying or distributing electric power characterised by its spatial reach or by the load
    • H02J2310/40—The network being an on-board power network, i.e. within a vehicle
    • H02J2310/44—The network being an on-board power network, i.e. within a vehicle for aircrafts
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/60—Other road transportation technologies with climate change mitigation effect
    • Y02T10/70—Energy storage systems for electromobility, e.g. batteries
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Definitions

  • Embodiments of the present invention relate to the field of drones, and more particularly to a battery control method, a battery control system, a drone, and a battery.
  • the battery is used as a power source for the drone, and is an indispensable part of the drone.
  • the battery fails during the flight of the drone, it may cause the drone to bomb, reducing the safety of the drone.
  • Embodiments of the present invention provide a battery control method, a battery control system, a drone, and a battery to improve the safety of the drone.
  • a first aspect of the embodiments of the present invention provides a battery control method, which is applied to a battery control system, and includes:
  • the battery is controlled to continue to supply power to the drone.
  • a second aspect of the embodiments of the present invention provides a battery control method, which is applied to a battery control system, and includes:
  • a switch of a power supply circuit connected to the battery for controlling power to the mobile platform is controlled according to status information of the processor.
  • a third aspect of the embodiments of the present invention provides a battery control system, the battery control system including:
  • One or more processors for:
  • the battery is controlled to continue to supply power to the drone.
  • a fourth aspect of the embodiments of the present invention provides a battery control system including: one or more processors, the processor is configured to:
  • a switch of a power supply circuit connected to the battery for controlling power to the mobile platform is controlled according to status information of the processor.
  • a fifth aspect of the embodiments of the present invention provides a battery control system including: a driving circuit for controlling a switch of a power supply circuit connected to a battery, wherein the battery is used to supply power to the movable platform;
  • One or more processors electrically coupled to the drive circuit for controlling the switch by the drive circuit
  • the drive circuit is used to:
  • a switch of a power supply circuit connected to the battery is controlled according to status information of the processor.
  • a sixth aspect of the embodiments of the present invention provides a drone, including:
  • a power system mounted to the fuselage for providing flight power
  • a flight controller in communication with the power system, for controlling the flight of the drone; and the battery control system of the third aspect, the fourth aspect, and the fifth aspect.
  • a seventh aspect of the embodiments of the present invention provides a drone, including:
  • a battery core mounted in the housing
  • the battery control system is electrically connected to the battery core.
  • the battery control method, the battery control system, the unmanned aerial vehicle and the battery obtained by the embodiment obtain the state information of the drone and the electrical parameter information of the battery through the battery control system, and determine the according to the electrical parameter information of the battery. Whether the battery is abnormal, when the drone is in a flight state, and the battery is in an abnormal state, the battery control system controls the battery to continue to supply power to the drone, so as to prevent the drone from being powered off during the flight. Falling ensures the safety of the drone.
  • FIG. 1 is a flowchart of a method for configuring a power system according to an embodiment of the present invention
  • FIG. 2 is a structural diagram of a drone according to an embodiment of the present invention.
  • FIG. 3 is a structural diagram of a drone according to an embodiment of the present invention.
  • FIG. 4 is a flowchart of a battery control method according to another embodiment of the present invention.
  • FIG. 5 is a structural diagram of a drone according to an embodiment of the present invention.
  • FIG. 6 is a flowchart of a battery control method according to another embodiment of the present invention.
  • FIG. 7 is a flowchart of a battery control method according to another embodiment of the present invention.
  • FIG. 8 is a structural diagram of a battery control system according to an embodiment of the present invention.
  • FIG. 9 is a structural diagram of a drone according to an embodiment of the present invention.
  • FIG. 10 is a structural diagram of a battery according to an embodiment of the present invention.
  • 919 battery control system
  • 902 support device
  • 904 shooting device
  • 1000 battery; 1001: housing; 1002: battery;
  • a component when referred to as being "fixed” to another component, it can be directly on the other component or the component can be present. When a component is considered to "connect” another component, it can be directly connected to another component or possibly a central component.
  • FIG. 1 is a flowchart of a battery control method according to an embodiment of the present invention.
  • the battery control method provided in this embodiment is applied to a battery control system. As shown in FIG. 1, the method in this embodiment may include:
  • Step S101 Obtain status information of the drone, and electrical parameter information of the battery, wherein the battery is used to supply power to the drone.
  • the battery control system is used to control the battery, and the battery is used to supply power to the drone.
  • the battery control system may be disposed in the drone or may be disposed in the casing of the battery.
  • the drone 20 includes a battery 21, a battery control system 22, and a flight controller 23, wherein the battery 21 is used to power the drone 20, and the battery control system 22 includes one or more processors.
  • the processor may be specifically a Micro Controller Unit (MCU).
  • the drone 30 includes a battery 31 and a flight controller 34, wherein the battery 31 includes a battery cell 32 and a battery control system 33.
  • the battery 31 is used to power the drone 30, and the battery control system 33 is electrically coupled to the battery core 32 and the flight controller 34, respectively.
  • the battery control system 22 can acquire status information of the drone 20 and electrical parameter information of the battery 21.
  • the acquiring the status information of the drone includes: receiving status information of the drone sent by the flight controller of the drone.
  • the flight controller 23 may determine the state information of the drone 20 based on the flight state parameters of the drone 20. Further, the flight controller 23 may transmit the state information of the drone 20 to the battery control system 22. After receiving the status information of the drone 20 transmitted by the flight controller 23, the battery control system 22 determines whether the drone 20 is in the flight state based on the status information of the drone 20.
  • battery control system 22 may also include an electrical parameter detection circuit that may be used to detect electrical parameter information for battery 21.
  • the electrical parameter information of the battery includes at least one of the following: voltage, current, output power, remaining power, and temperature of the battery.
  • Step S102 Determine, according to electrical parameter information of the battery, whether the battery is abnormal.
  • the processor in the battery control system 22 can determine whether the battery 21 is abnormal according to the electrical parameter information of the battery 21, for example, determining whether the voltage of the battery 21 is less than a preset voltage value, and determining whether the temperature of the battery 21 is greater than a preset.
  • the temperature value determines whether the current of the battery 21 is greater than a preset current value, and determines whether the power of the battery 21 is greater than a rated power or the like.
  • Step S103 When the state information of the drone indicates that the drone is in a flying state, and the battery is in an abnormal state, the battery is controlled to continue to supply power to the drone.
  • the battery control system 22 determines that the drone 20 is in flight and the battery 21 is in an abnormal state
  • the battery control system 22 controls the battery 21 to continue to supply power to the drone 20. It will be appreciated that when the battery control system 22 determines that the drone 20 is in flight and the battery 21 is in an abnormal state, if the battery 21 does not continue to power the drone 20, the drone 20 may fall and be damaged.
  • the battery control system 22 controls the battery 21 to continue to power the drone 20 to ensure that the drone 20 does not fall immediately and is damaged.
  • the battery control system 22 can transmit the abnormal state information of the battery 21 to the flight controller 23, and the flight controller 23 can control the drone 20 to descend according to the abnormal state information of the battery 21.
  • determining whether the battery is abnormal according to electrical parameter information of the battery includes: determining, according to a voltage of the battery, whether the battery is under voltage.
  • the battery control system 22 determines that the voltage of the battery 21 is less than the preset voltage value, the battery control system 22 determines that the battery 21 is in an undervoltage condition.
  • controlling the battery to continue to supply power to the drone including:
  • the status information of the drone indicates that the drone is in a flight state, and when the battery is under voltage, the battery is controlled to continue to supply power to the drone.
  • the battery control system 22 determines that the drone 20 is in flight and the battery 21 is in an undervoltage condition, the battery control system 22 controls the battery 21 to continue to power the drone 20.
  • controlling the battery to continue to supply power to the drone comprises: controlling a power supply circuit connected to the battery to continue to supply power to the drone.
  • 24 denotes a power supply circuit connected to the battery 21, and the battery 21 supplies power to the drone 20 through the power supply circuit 24.
  • the battery control system 22 controlling the battery 21 to continue to power the drone 20 is that the battery control system 22 controls the power supply circuit 24 coupled to the battery 21 to continue to power the drone 20.
  • controlling the power supply circuit connected to the battery continues to supply power to the drone, comprising: controlling a switch closure of a power supply circuit connected to the battery, so that the power supply circuit continues to the Man-machine power supply.
  • the power supply circuit 24 includes a switch 25, which may be a metal oxide semiconductor (MOS) tube.
  • a switch 25 when the switch 25 is closed, the battery 21 can supply power to the drone 20 through the power supply circuit 24; when the switch 25 is turned off, the battery 21 cannot supply power to the drone 20 through the power supply circuit 24.
  • MOS metal oxide semiconductor
  • the battery control system 22 determines that the drone 20 is in flight and the battery 21 is in an undervoltage condition, the battery control system 22 can be closed by the control switch 25 to cause the battery 21 to continue to power the drone 20 through the power supply circuit 24. .
  • the method further includes: when the status information of the drone indicates that the drone is in a non-flying state, and the battery is in an abnormal state, controlling the battery to stop to the Man-machine power supply.
  • the battery control system 22 determines that the drone 20 is in a non-flying state, for example, the drone 20 is performing data copying, and the battery control system 22 determines that the battery 21 is in an abnormal state, in order to protect the battery from damage.
  • the battery control system 22 can control the battery 21 to stop supplying power to the drone 20.
  • controlling the battery to stop supplying power to the drone including: when the The status information of the man machine indicates that the drone is in a non-flying state, and when the battery is under voltage, the battery is controlled to stop supplying power to the drone.
  • the battery control system 22 determines that the battery 21 is in an undervoltage condition.
  • the battery control system 22 determines that the drone 20 is in a non-flying state, such as when the drone 20 is performing a data copy, and the battery control system 22 determines that the battery 21 is in an undervoltage condition, in order to avoid the battery 21 being subjected to an undervoltage condition.
  • the battery control system 22 can control the battery 21 to stop supplying power to the drone 20.
  • the controlling the battery to stop supplying power to the drone includes: controlling a power supply circuit connected to the battery to stop supplying power to the drone.
  • the battery control system 22 controlling the battery 21 to stop powering the drone 20 is that the battery control system 22 controls the power supply circuit 24 connected to the battery 21 to stop supplying power to the drone 20.
  • the controlling the power supply circuit connected to the battery to stop supplying power to the drone comprising: controlling a switch of a power supply circuit connected to the battery to be disconnected, so that the power supply circuit stops supplying power to the drone .
  • the battery control system 22 determines that the drone 20 is in flight and the battery 21 is in an undervoltage condition, the battery control system 22 can be opened by the control switch 25 to cause the power supply circuit 24 to stop supplying power to the drone 20.
  • the battery control system acquires state information of the drone, and electrical parameter information of the battery, and determines, according to the electrical parameter information of the battery, whether the battery is abnormal, when the drone is in a flight state, and the battery When in an abnormal state, the battery control system controls the battery to continue to supply power to the drone, preventing the drone from falling due to battery power failure during flight, thereby ensuring the safety of the drone.
  • FIG. 4 is a flowchart of a battery control method according to another embodiment of the present invention. As shown in FIG. 4, on the basis of the embodiment shown in FIG. 1, the method in this embodiment may further include:
  • Step S401 Detect status information of a processor in the battery control system.
  • battery control system 22 includes a processor 26 and a drive circuit 27, wherein the processor includes a micro control unit MCU.
  • the drive circuit 27 is for controlling the switch 25 of the power supply circuit 24 connected to the battery 21.
  • the detecting status information of the processor in the battery control system includes: a driving circuit in the battery control system detects whether a processor in the battery control system is abnormal, and the driving circuit is configured to control connection with a battery The switch of the power supply circuit.
  • drive circuit 27 in battery control system 22 detects if processor 26 is abnormal.
  • Step S402 controlling a switch of the power supply circuit connected to the battery according to the state information of the processor.
  • the drive circuit 27 can control the switch 25 of the power supply circuit 24 connected to the battery 21 according to the state information of the processor 26.
  • controlling, according to the state information of the processor, a switch of the power supply circuit connected to the battery comprising: if the processor is in an abnormal state, the driving circuit controls a power supply circuit connected to the battery The switch is closed to cause the power supply circuit to continue to power the drone.
  • the drive circuit 27 can control the switch 25 of the power supply circuit 24 connected to the battery 21 to be closed, so that the power supply circuit 24 continues to supply power to the drone 20.
  • the drive circuit in the battery control system detects whether the processor in the battery control system is abnormal, including: the drive circuit in the battery control system detects whether the processor in the battery control system is in a reset state.
  • drive circuit 27 in battery control system 22 can detect if processor 26 is in a reset state.
  • the driving circuit controls the switch of the power supply circuit connected to the battery to be closed, so that the power supply circuit continues to supply power to the drone, including: if the processing The device is in a reset state, and the drive circuit controls the switch of the power supply circuit connected to the battery to be closed, so that the power supply circuit continues to supply power to the drone.
  • the drive circuit 27 when the drive circuit 27 determines that the processor 26 is in the reset state, the drive circuit 27 can control the switch 25 of the power supply circuit 24 connected to the battery 21 to be closed, so that the power supply circuit 24 continues to supply power to the drone 20, avoiding the processor.
  • the battery 21 is subjected to the disturbance reset, the battery 21 immediately stops supplying power to the drone 20, and the drone 20 that causes the flight state is forced to bomb.
  • the flight controller 23 may not be in normal communication with the processor 26, at which time the flight controller 23 may control the drone 20 to descend to avoid the bombing.
  • the controlling according to the state information of the processor, the switch of the power supply circuit connected to the battery, comprising: when the processor is in an upgrade state, and the current of the battery is greater than or equal to a current threshold, the control The switch of the power supply circuit connected to the battery is disconnected to stop the power supply circuit from supplying power.
  • the processor 26 can also detect its status information. For example, the processor 26 can also detect whether it is in an upgrade state. When the processor 26 is in an upgrade state, the upgrade loader can also detect the voltage and/or current of the battery 21. Further, the processor 26 can also control the switch 25 of the power supply circuit 24 connected to the battery 21 according to the voltage and/or current of the battery 21.
  • the processor 26 controls the switch 25 of the power supply circuit 24 connected to the battery 21 to be turned off, so that the power supply circuit 24 stops supplying power. To prevent the battery 21 from being damaged due to overcurrent.
  • controlling according to the state information of the processor, the switch of the power supply circuit connected to the battery, comprising: when the processor is in an upgrade state, and the voltage of the battery is less than or equal to a first voltage threshold And controlling a switch of the power supply circuit connected to the battery to be disconnected, so that the power supply circuit stops supplying power.
  • the processor 26 controls the switch 25 of the power supply circuit 24 connected to the battery 21 to be turned off, so that the power supply circuit 24 is turned off.
  • the power supply is stopped to prevent the battery 21 from being damaged due to undervoltage.
  • the first voltage threshold is 3.2V.
  • the method further includes the following steps as shown in FIG. 6:
  • Step S601 Detect status information of the battery.
  • the processor 26 can also detect status information of the battery 21. For example, when the voltage of the battery 21 is less than or equal to 3.2V, the battery 21 needs to be charged. The processor 26 can specifically detect if the battery 21 is in a charged state.
  • the battery 21 when the processor 26 is in the upgrade state, the battery 21 is powered outward; when the battery 21 is connected to the charger, the battery 21 starts to be charged and does not supply power.
  • the battery 21 is not limited to powering the drone, and can also supply power to other loads.
  • Step S602 When the battery is in a charging state, and the voltage of the battery is greater than or equal to the second voltage threshold, the switch of the power supply circuit connected to the battery is controlled to be closed, so that the power supply circuit supplies power externally.
  • the processor 26 when the processor 26 is in an upgraded state, the battery 21 is powered externally, the voltage of the battery 21 is continuously decreasing, and when the voltage of the battery 21 is less than or equal to, for example, 3.2 V, the processor 26 controls the power supply circuit 24 connected to the battery 21.
  • the switch 25 is turned off, and at this time, the battery 21 cannot be powered outward to prevent the battery 21 from being damaged.
  • the voltage of the battery 21 is continuously increased.
  • the processor 26 controls the switch 25 of the power supply circuit 24 connected to the battery 21 to be closed. At this time, the battery 21 can supply power to the outside.
  • Step S603 when the battery is in a charging state, and the voltage of the battery is greater than or equal to a third voltage threshold, controlling a switch of the charging circuit connected to the battery to be disconnected, so that the charging circuit stops Charging batteries.
  • the processor 26 controls the switch 25 of the power supply circuit 24 connected to the battery 21 to be closed. At this time, the battery 21 can supply power to the outside. If the battery 21 continues to be charged at this time, the voltage of the battery 21 will continue to increase.
  • the processor 26 can also control the battery 21 The switch of the connected charging circuit is turned off.
  • the battery 21 Since the battery 21 is connected to the charger through the charging circuit, when the processor 26 controls the switch of the charging circuit connected to the battery 21 to be disconnected, the connection between the control battery 21 and the charger is disconnected, so that the charger is stopped.
  • the battery 21 is continuously charged to prevent the battery 21 from being over- or over-temperature during charging to affect the performance of the battery 21.
  • the embodiment controls the state information of the processor in the battery control system, controls the switch of the power supply circuit connected to the battery according to the state information of the processor, and prevents the battery from immediately stopping when the processor is subjected to the interference reset.
  • the drone that is powered by the drone is forced to bomb the aircraft; in addition, when the processor is in an upgrade state and the battery is under voltage or overcurrent, the processor controls the switch of the power supply circuit connected to the battery to be disconnected, The power supply circuit is stopped from being powered, and the battery is prevented from being damaged due to undervoltage or overcurrent. On the basis of ensuring safe flight of the drone, the battery can be prevented from being damaged.
  • the battery voltage is detected during the charging process by the battery. When the battery is over-pressurized, the switch of the charging circuit connected to the battery is controlled to be disconnected, so that the charging circuit stops charging the battery to prevent the battery from being over-damaged and damaged.
  • FIG. 7 is a flowchart of a battery control method according to another embodiment of the present invention. As shown in FIG. 7, the battery control method in this embodiment is applied to a battery control system. The method in this embodiment may include:
  • Step S701 Detect status information of a processor in the battery control system.
  • battery control system 22 includes a processor 26 and a drive circuit 27, wherein the processor includes a micro control unit MCU.
  • the drive circuit 27 is for controlling the switch 25 of the power supply circuit 24 connected to the battery 21.
  • the detecting status information of the processor in the battery control system includes: a driving circuit in the battery control system detects whether a processor in the battery control system is abnormal, and the driving circuit is configured to control connection with a battery The switch of the power supply circuit.
  • drive circuit 27 in battery control system 22 detects if processor 26 is abnormal.
  • Step S702 Control, according to the state information of the processor, a switch of a power supply circuit connected to the battery, wherein the battery is used to supply power to the movable platform.
  • the driving circuit 27 can control the switch 25 of the power supply circuit 24 connected to the battery 21 according to the state information of the processor 26, and the battery 21 is used to supply power to the movable platform.
  • the movable platform includes no one. machine.
  • the controlling according to the state information of the processor, the switch of the power supply circuit connected to the battery, comprising: if the processor is in an abnormal state, the driving circuit controls a switch of a power supply circuit connected to the battery Closing to cause the power supply circuit to continue to power the movable platform.
  • the drive circuit 27 can control the switch 25 of the power supply circuit 24 connected to the battery 21 to be closed, so that the power supply circuit 24 continues to supply power to the drone 20.
  • the drive circuit in the battery control system detects whether the processor in the battery control system is abnormal, including: the drive circuit in the battery control system detects whether the processor in the battery control system is in a reset state.
  • drive circuit 27 in battery control system 22 can detect if processor 26 is in a reset state.
  • the driving circuit controls the switch of the power supply circuit connected to the battery to be closed, so that the power supply circuit continues to supply power to the movable platform, including: if the processing The device is in a reset state, and the drive circuit controls the switch of the power supply circuit connected to the battery to be closed, so that the power supply circuit continues to supply power to the movable platform.
  • the drive circuit 27 when the drive circuit 27 determines that the processor 26 is in the reset state, the drive circuit 27 can control the switch 25 of the power supply circuit 24 connected to the battery 21 to be closed, so that the power supply circuit 24 continues to supply power to the drone 20, avoiding the processor.
  • the battery 21 is subjected to the disturbance reset, the battery 21 immediately stops supplying power to the drone 20, and the drone 20 that causes the flight state is forced to bomb.
  • the flight controller 23 may not be in normal communication with the processor 26, at which time the flight controller 23 may control the drone 20 to descend to avoid the bombing.
  • the controlling according to the state information of the processor, the switch of the power supply circuit connected to the battery, comprising: when the processor is in an upgrade state, and the current of the battery is greater than or equal to a current threshold, the control The switch of the power supply circuit connected to the battery is disconnected to stop the power supply circuit from supplying power.
  • the processor 26 can also detect its status information. For example, the processor 26 can also detect whether it is in an upgrade state. When the processor 26 is in an upgrade state, the upgrade loader can also detect the voltage and/or current of the battery 21. Further, the processor 26 can also control the switch 25 of the power supply circuit 24 connected to the battery 21 according to the voltage and/or current of the battery 21.
  • the processor 26 controls the switch 25 of the power supply circuit 24 connected to the battery 21 to be turned off, so that the power supply circuit 24 stops supplying power. To prevent the battery 21 from being damaged due to overcurrent.
  • controlling according to the state information of the processor, the switch of the power supply circuit connected to the battery, comprising: when the processor is in an upgrade state, and the voltage of the battery is less than or equal to a first voltage threshold And controlling a switch of the power supply circuit connected to the battery to be disconnected, so that the power supply circuit stops supplying power.
  • the processor 26 controls the switch 25 of the power supply circuit 24 connected to the battery 21 to be turned off, so that the power supply circuit 24 is turned off.
  • the power supply is stopped to prevent the battery 21 from being damaged due to undervoltage.
  • the first voltage threshold is 3.2V.
  • the embodiment controls the state information of the processor in the battery control system, controls the switch of the power supply circuit connected to the battery according to the state information of the processor, and prevents the battery from immediately stopping when the processor is subjected to the interference reset.
  • the drone that is powered by the drone is forced to bomb the aircraft; in addition, when the processor is in an upgrade state and the battery is under voltage or overcurrent, the processor controls the switch of the power supply circuit connected to the battery to be disconnected, The power supply circuit is stopped from being powered, and the battery is prevented from being damaged due to undervoltage or overcurrent. On the basis of ensuring safe flight of the drone, the battery can be prevented from being damaged.
  • FIG. 8 is a structural diagram of a battery control system according to an embodiment of the present invention.
  • the battery control system 80 includes one or more processors 81.
  • the processor 81 is configured to: acquire state information of the drone, and electrical parameter information of the battery, where the battery is used to supply power to the drone; and determine whether the battery is abnormal according to electrical parameter information of the battery; When the status information of the drone indicates that the drone is in a flight state, and the battery is in an abnormal state, the battery is controlled to continue to supply power to the drone.
  • the electrical parameter information of the battery includes at least one of the following: voltage, current, output power, remaining power, and temperature of the battery.
  • the processor 81 determines, according to the electrical parameter information of the battery, whether the battery is abnormal, specifically, determining, according to the voltage of the battery, whether the battery is under voltage; when the The status information indicates that the drone is in a flight state, and when the battery is in an abnormal state, the processor 81 controls the battery to continue to supply power to the drone.
  • the method is specifically configured to: control a power supply circuit connected to the battery to continue to supply power to the drone.
  • the method is: controlling a switch of a power supply circuit connected to the battery to be closed, so that the power supply circuit continues Powering the drone.
  • the processor 81 is further configured to: when the status information of the drone indicates that the drone is in a non-flying state, and the battery is in an abnormal state, control the battery to stop to the unmanned Machine power supply.
  • the processor 81 controls the battery to stop supplying power to the drone.
  • the method is specifically configured to: control a power supply circuit connected to the battery to stop supplying power to the drone.
  • the processor 81 controls the power supply circuit connected to the battery to stop supplying power to the drone
  • the processor 81 is specifically configured to: control a switch of the power supply circuit connected to the battery to be disconnected, so that the power supply circuit Stop supplying power to the drone.
  • the processor 81 when acquiring the status information of the UAV, is specifically configured to: receive status information of the UAV sent by the flight controller of the UAV.
  • the battery control system 80 further includes: a driving circuit 82, the driving circuit 82 is electrically connected to the processor 81, and the driving circuit 82 is configured to: detect status information of the processor in the battery control system; Status information controls the switching of the power supply circuit connected to the battery.
  • the driving circuit 82 detects the state information of the processor in the battery control system, specifically, the driving circuit 82 detects whether the processor in the battery control system is abnormal; and the driving circuit 82 is configured according to the processor 81.
  • State information when controlling the switch of the power supply circuit connected to the battery, specifically for: if the processor 81 is in an abnormal state, the drive circuit 82 controls the switch of the power supply circuit connected to the battery to be closed, so that the power supply The circuit continues to power the processor 81 to the drone.
  • driver circuit 82 detects whether the processor in the battery control system is abnormal, specifically, detecting whether the processor in the battery control system is in a reset state; if the processor 81 is in a reset state, driving Circuitry 82 controls the closing of the switch of the power supply circuit coupled to the battery to cause the power supply circuit to continue to power the drone.
  • the processor 81 is further configured to: detect state information of the processor 81; and control a switch of the power supply circuit connected to the battery according to the state information of the processor 81.
  • the processor 81 controls the switch of the power supply circuit connected to the battery according to the state information of the processor 81, specifically, when the processor 81 is in an upgrade state, and the current of the battery is greater than or equal to the current. At the threshold, the switch of the power supply circuit connected to the battery is controlled to be disconnected, so that the power supply circuit stops supplying power.
  • the processor 81 controls the switch of the power supply circuit connected to the battery according to the state information of the processor 81, specifically, when the processor 81 is in an upgrade state, and the voltage of the battery is less than or equal to the first At a voltage threshold, the switch of the power supply circuit connected to the battery is controlled to be disconnected to stop the power supply circuit from supplying power.
  • the processor 81 is further configured to: detect status information of the battery; when the battery is in a charging state, and the voltage of the battery is greater than or equal to a second voltage threshold, controlling power supply connected to the battery The switch of the circuit is closed to allow the power supply circuit to supply power to the outside.
  • the processor 81 is further configured to: when the battery is in a charging state, and the voltage of the battery is greater than or equal to a third voltage threshold, control a switch of the charging circuit connected to the battery to be disconnected, so that The charging circuit stops charging the battery.
  • the processor 81 includes a micro control unit MCU.
  • the battery control system acquires state information of the drone, and electrical parameter information of the battery, and determines, according to the electrical parameter information of the battery, whether the battery is abnormal, when the drone is in a flight state, and the battery When in an abnormal state, the battery control system controls the battery to continue to supply power to the drone, preventing the drone from falling due to battery power failure during flight, thereby ensuring the safety of the drone.
  • Embodiments of the present invention provide a battery control system.
  • the battery control system 80 includes one or more processors 81 for detecting status information of the processor 81 and controlling the switching of the power supply circuit connected to the battery according to the status information of the processor 81.
  • the battery is used to power a mobile platform.
  • the processor 81 controls the switch of the power supply circuit connected to the battery according to the state information of the processor 81, specifically, when the processor 81 is in an upgrade state, and the current of the battery is greater than or equal to a current threshold. And controlling a switch of the power supply circuit connected to the battery to be disconnected, so that the power supply circuit stops supplying power.
  • the processor 81 controls the switch of the power supply circuit connected to the battery according to the state information of the processor 81, specifically, when the processor 81 is in an upgrade state, and the voltage of the battery is less than or equal to the first voltage. At the threshold, the switch of the power supply circuit connected to the battery is controlled to be disconnected, so that the power supply circuit stops supplying power.
  • the movable platform comprises a drone.
  • the embodiment controls the state information of the processor in the battery control system, controls the switch of the power supply circuit connected to the battery according to the state information of the processor, and prevents the battery from immediately stopping when the processor is subjected to the interference reset.
  • the drone that is powered by the drone is forced to bomb the aircraft; in addition, when the processor is in an upgrade state and the battery is under voltage or overcurrent, the processor controls the switch of the power supply circuit connected to the battery to be disconnected, The power supply circuit is stopped from being powered, and the battery is prevented from being damaged due to undervoltage or overcurrent. On the basis of ensuring safe flight of the drone, the battery can be prevented from being damaged.
  • the battery control system 80 includes one or more processors 81 and a drive circuit 82.
  • the processor 81 is electrically coupled to a drive circuit 82 for controlling a switch of a power supply circuit connected to the battery.
  • the battery is used to supply power to the movable platform; the processor 81 is configured to control the switch by the driving circuit 82; the driving circuit 82 is configured to: detect status information of the processor in the battery control system; and according to status information of the processor 81 , controls the switch of the power supply circuit connected to the battery.
  • the driving circuit 82 detects the state information of the processor in the battery control system
  • the method is specifically configured to: detect whether the processor in the battery control system is abnormal; and the driving circuit 82 is configured according to the state information of the processor 81.
  • the switch of the power supply circuit connected to the battery is controlled, specifically, if the processor 81 is in an abnormal state, the drive circuit 82 controls the switch of the power supply circuit connected to the battery to be closed, so that the power supply circuit continues to the Powered by mobile platforms.
  • driver circuit 82 detects whether the processor in the battery control system is abnormal, specifically, detecting whether the processor in the battery control system is in a reset state; if the processor 81 is in a reset state, driving Circuitry 82 controls the closing of the switch of the power supply circuit coupled to the battery to cause the power supply circuit to continue to power the movable platform.
  • the movable platform comprises a drone.
  • the embodiment controls the state information of the processor in the battery control system, controls the switch of the power supply circuit connected to the battery according to the state information of the processor, and prevents the battery from immediately stopping when the processor is subjected to the interference reset.
  • the drone that is powered by the drone is forced to bomb the aircraft; in addition, when the processor is in an upgrade state and the battery is under voltage or overcurrent, the processor controls the switch of the power supply circuit connected to the battery to be disconnected, The power supply circuit is stopped from being powered, and the battery is prevented from being damaged due to undervoltage or overcurrent. On the basis of ensuring safe flight of the drone, the battery can be prevented from being damaged.
  • FIG. 9 is a structural diagram of a drone according to an embodiment of the present invention.
  • the drone 900 includes: a fuselage, a power system, a flight controller 918, and a battery control system 919, and the power system includes the following: At least one of: a motor 907, a propeller 906, and an electronic governor 917, the power system being mounted to the fuselage for providing flight power; the flight controller 918 being communicatively coupled to the power system for controlling the unmanned Flight.
  • the drone 900 further includes: a supporting device 902 and a photographing device 904, wherein the supporting device 902 may specifically be a pan/tilt.
  • the battery control system acquires state information of the drone, and electrical parameter information of the battery, and determines, according to the electrical parameter information of the battery, whether the battery is abnormal, when the drone is in a flight state, and the battery When in an abnormal state, the battery control system controls the battery to continue to supply power to the drone, preventing the drone from falling due to battery power failure during flight, thereby ensuring the safety of the drone.
  • FIG. 10 is a structural diagram of a battery according to an embodiment of the present invention.
  • the battery 1000 includes a housing 1001, a battery 1002, and a battery control system 1003.
  • the battery cell 1002 is mounted in the housing 1001
  • the battery control system 1003 is mounted in the housing 1001
  • the battery control system 1003 is electrically connected to the battery cell 1002.
  • the specific principles and implementations of the battery control system 1003 are similar to the above embodiments, and are not described herein again.
  • the battery control system acquires state information of the drone, and electrical parameter information of the battery, and determines, according to the electrical parameter information of the battery, whether the battery is abnormal, when the drone is in a flight state, and the battery When in an abnormal state, the battery control system controls the battery to continue to supply power to the drone, preventing the drone from falling due to battery power failure during flight, thereby ensuring the safety of the drone.
  • the disclosed apparatus and method may be implemented in other manners.
  • the device embodiments described above are merely illustrative.
  • the division of the unit is only a logical function division.
  • there may be another division manner for example, multiple units or components may be combined or Can be integrated into another system, or some features can be ignored or not executed.
  • the mutual coupling or direct coupling or communication connection shown or discussed may be an indirect coupling or communication connection through some interface, device or unit, and may be in an electrical, mechanical or other form.
  • the units described as separate components may or may not be physically separated, and the components displayed as units may or may not be physical units, that is, may be located in one place, or may be distributed to multiple network units. Some or all of the units may be selected according to actual needs to achieve the purpose of the solution of the embodiment.
  • each functional unit in each embodiment of the present invention may be integrated into one processing unit, or each unit may exist physically separately, or two or more units may be integrated into one unit.
  • the above integrated unit can be implemented in the form of hardware or in the form of hardware plus software functional units.
  • the above-described integrated unit implemented in the form of a software functional unit can be stored in a computer readable storage medium.
  • the above software functional unit is stored in a storage medium and includes instructions for causing a computer device (which may be a personal computer, a server, or a network device, etc.) or a processor to perform the methods of the various embodiments of the present invention. Part of the steps.
  • the foregoing storage medium includes: a U disk, a mobile hard disk, a read-only memory (ROM), a random access memory (RAM), a magnetic disk, or an optical disk, and the like, which can store program codes. .

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Abstract

一种电池控制方法、电池控制***、无人机及电池，该方法包括：获取无人机的状态信息，以及电池的电参数信息，其中，所述电池用于给所述无人机供电（S101）；根据所述电池的电参数信息，确定所述电池是否异常（S102）；当所述无人机的状态信息表示所述无人机处于飞行状态，且所述电池处于异常状态时，控制所述电池继续给所述无人机供电（S103）。通过该方法避免了无人机在飞行过程中由于电池断电而坠落，保证了无人机的安全性。

Description

电池控制方法、电池控制***、无人机及电池 技术领域
本发明实施例涉及无人机领域，尤其涉及一种电池控制方法、电池控制***、无人机及电池。
背景技术
现有技术中电池作为无人机的动力电源，是无人机不可或缺的部分。但是，在无人机飞行过程中，如果电池出现故障，可能会导致无人机炸机，降低了无人机的安全性。
发明内容
本发明实施例提供一种电池控制方法、电池控制***、无人机及电池，以提高无人机的安全性。
本发明实施例的第一方面是提供一种电池控制方法，应用于电池控制***，包括：
获取无人机的状态信息，以及电池的电参数信息，其中，所述电池用于给所述无人机供电；
根据所述电池的电参数信息，确定所述电池是否异常；
当所述无人机的状态信息表示所述无人机处于飞行状态，且所述电池处于异常状态时，控制所述电池继续给所述无人机供电。
本发明实施例的第二方面是提供一种电池控制方法，应用于电池控制***，包括：
检测所述电池控制***中的处理器的状态信息；
根据所述处理器的状态信息，控制与电池连接的供电电路的开关，所述电池用于给可移动平台供电。
本发明实施例的第三方面是提供一种电池控制***，所述电池控制***包括：
一个或多个处理器，所述处理器用于：
获取无人机的状态信息，以及电池的电参数信息，所述电池用于给所述无人机供电；
根据所述电池的电参数信息，确定所述电池是否异常；
当所述无人机的状态信息表示所述无人机处于飞行状态，且所述电池处于异常状态时，控制所述电池继续给所述无人机供电。
本发明实施例的第四方面是提供一种电池控制***，包括：一个或多个处理器，所述处理器用于：
检测所述处理器的状态信息；
根据所述处理器的状态信息，控制与电池连接的供电电路的开关，所述电池用于给可移动平台供电。
本发明实施例的第五方面是提供一种电池控制***，包括：驱动电路，所述驱动电路用于控制与电池连接的供电电路的开关，所述电池用于给可移动平台供电；
一个或多个处理器，所述处理器与所述驱动电路电连接，用于通过所述驱动电路控制所述开关；
所述驱动电路用于：
检测所述电池控制***中的处理器的状态信息；
根据所述处理器的状态信息，控制与电池连接的供电电路的开关。
本发明实施例的第六方面是提供一种无人机，包括：
机身；
动力***，安装在所述机身，用于提供飞行动力；
飞行控制器，与所述动力***通讯连接，用于控制所述无人机飞行；以及上述第三方面、第四方面、第五方面所述的电池控制***。
本发明实施例的第七方面是提供一种无人机，包括：
壳体；
电芯，安装在所述壳体内；以及
上述第三方面、第四方面、第五方面所述的电池控制***，电池控制***安装在所述壳体内；
其中，所述电池控制***与所述电芯电连接。
本实施例提供的电池控制方法、电池控制***、无人机及电池，通过 电池控制***获取无人机的状态信息，以及电池的电参数信息，根据所述电池的电参数信息，确定所述电池是否异常，当无人机处于飞行状态，且所述电池处于异常状态时，电池控制***控制所述电池继续给所述无人机供电，避免无人机在飞行过程中由于电池断电而坠落，保证了无人机的安全性。
附图说明
为了更清楚地说明本发明实施例中的技术方案，下面将对实施例描述中所需要使用的附图作一简单地介绍，显而易见地，下面描述中的附图是本发明的一些实施例，对于本领域普通技术人员来讲，在不付出创造性劳动性的前提下，还可以根据这些附图获得其他的附图。
图1为本发明实施例提供的动力***配置方法的流程图；
图2为本发明实施例提供的无人机的结构图；
图3为本发明实施例提供的无人机的结构图；
图4为本发明另一实施例提供的电池控制方法的流程图；
图5为本发明实施例提供的无人机的结构图；
图6为本发明另一实施例提供的电池控制方法的流程图；
图7为本发明另一实施例提供的电池控制方法的流程图；
图8为本发明实施例提供的电池控制***的结构图；
图9为本发明实施例提供的无人机的结构图；
图10为本发明实施例提供的电池的结构图。
附图标记：
20：无人机；         21：电池；         22：电池控制***；
23：飞行控制器；     24：供电电路；      25：开关；
30：无人机；         31：电池；         32：电芯；
33：电池控制***；    34：飞行控制器；     26：处理器；
27：驱动电路；        80：电池控制***；   81：处理器；
82：驱动电路；        900：无人机；        907：电机；
906：螺旋桨；         917：电子调速器；    918：飞行控制器；
919：电池控制***；     902：支撑设备；      904：拍摄设备
1000：电池；           1001：壳体；         1002：电芯；
1003：电池控制***。
具体实施方式
下面将结合本发明实施例中的附图，对本发明实施例中的技术方案进行清楚地描述，显然，所描述的实施例仅仅是本发明一部分实施例，而不是全部的实施例。基于本发明中的实施例，本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例，都属于本发明保护的范围。
需要说明的是，当组件被称为“固定于”另一个组件，它可以直接在另一个组件上或者也可以存在居中的组件。当一个组件被认为是“连接”另一个组件，它可以是直接连接到另一个组件或者可能同时存在居中组件。
除非另有定义，本文所使用的所有的技术和科学术语与属于本发明的技术领域的技术人员通常理解的含义相同。本文中在本发明的说明书中所使用的术语只是为了描述具体的实施例的目的，不是旨在于限制本发明。本文所使用的术语“及/或”包括一个或多个相关的所列项目的任意的和所有的组合。
下面结合附图，对本发明的一些实施方式作详细说明。在不冲突的情况下，下述的实施例及实施例中的特征可以相互组合。
本发明实施例提供一种电池控制方法。图1为本发明实施例提供的电池控制方法的流程图。本实施例提供的电池控制方法应用于电池控制***。如图1所示，本实施例中的方法，可以包括：
步骤S101、获取无人机的状态信息，以及电池的电参数信息，其中，所述电池用于给所述无人机供电。
在本实施例中，电池控制***用于控制电池，该电池用于给无人机供电，该电池控制***可以设置在无人机中，也可以设置在电池的壳体中。
如图2所示，无人机20包括电池21、电池控制***22和飞行控制器23，其中，电池21用于给无人机20供电，电池控制***22包括一个或多个处理器，该处理器具体可以是微控制单元(Micro Controller Unit，简称MCU)。
如图3所示，无人机30包括电池31和飞行控制器34，其中，电池 31包括电芯32和电池控制***33。电池31用于给无人机30供电，电池控制***33分别与电芯32和飞行控制器34电连接。
本实施例以图2所示的情况为例进行示意性说明。如图2所示，电池控制***22可获取无人机20的状态信息，以及电池21的电参数信息。
所述获取无人机的状态信息，包括：接收所述无人机的飞行控制器发送的所述无人机的状态信息。例如，飞行控制器23可根据无人机20的飞行状态参数确定出无人机20的状态信息，进一步的，飞行控制器23可将无人机20的状态信息发送给电池控制***22。电池控制***22接收飞行控制器23发送的无人机20的状态信息后，根据无人机20的状态信息确定无人机20是否处于飞行状态。
另外，电池控制***22还可以包括电参数检测电路，该电参数检测电路可用于检测电池21的电参数信息。
可选的，所述电池的电参数信息包括如下至少一种：所述电池的电压、电流、输出功率、剩余电量、温度。
步骤S102、根据所述电池的电参数信息，确定所述电池是否异常。
可选的，电池控制***22内的处理器可根据电池21的电参数信息，确定电池21是否异常，例如，确定电池21的电压是否小于预设电压值，确定电池21的温度是否大于预设温度值，确定电池21的电流是否大于预设电流值，确定电池21的功率是否大于额定功率等。
步骤S103、当所述无人机的状态信息表示所述无人机处于飞行状态，且所述电池处于异常状态时，控制所述电池继续给所述无人机供电。
具体的，当电池控制***22确定出无人机20处于飞行状态，且电池21处于异常状态时，电池控制***22控制电池21继续给无人机20供电。可以理解，当电池控制***22确定出无人机20处于飞行状态，且电池21处于异常状态时，如果电池21不继续给无人机20供电，则无人机20可能会坠落而损坏。电池控制***22控制电池21继续给无人机20供电可保证无人机20不会立即坠落而损坏。此时，电池控制***22可以将电池21的异常状态信息发送给飞行控制器23，飞行控制器23可根据电池21的异常状态信息，控制无人机20下降。
具体的，所述根据所述电池的电参数信息，确定所述电池是否异常， 包括：根据所述电池的电压，确定所述电池是否欠压。
如果电池控制***22确定电池21的电压小于预设电压值，则电池控制***22确定电池21处于欠压状态。
具体的，所述当所述无人机的状态信息表示所述无人机处于飞行状态，且所述电池处于异常状态时，控制所述电池继续给所述无人机供电，包括：当所述无人机的状态信息表示所述无人机处于飞行状态，且所述电池欠压时，控制所述电池继续给所述无人机供电。
例如，当电池控制***22确定出无人机20处于飞行状态，且电池21处于欠压状态时，电池控制***22控制电池21继续给无人机20供电。
可选的，所述控制所述电池继续给所述无人机供电，包括：控制与所述电池连接的供电电路继续给所述无人机供电。
如图2所示，24表示与电池21连接的供电电路，电池21通过供电电路24给无人机20供电。可选的，电池控制***22控制电池21继续给无人机20供电的一种可行的实现方式是：电池控制***22控制与电池21连接的供电电路24继续给无人机20供电。
可选的，所述控制与所述电池连接的供电电路继续给所述无人机供电，包括：控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述无人机供电。
如图2所示，供电电路24包括开关25，开关25具体可以是金属氧化物半导体(metal oxide semiconductor，简称MOS)管。可选的，当开关25闭合时，电池21可通过供电电路24给无人机20供电；当开关25断开时，电池21无法通过供电电路24给无人机20供电。
当电池控制***22确定出无人机20处于飞行状态，且电池21处于欠压状态时，电池控制***22可通过控制开关25闭合，以使电池21通过供电电路24给无人机20继续供电。
在其他实施例中，所述方法还包括：当所述无人机的状态信息表示所述无人机处于非飞行状态，且所述电池处于异常状态时，控制所述电池停止给所述无人机供电。
如图2所示，当电池控制***22确定出无人机20处于非飞行状态，例如无人机20在进行数据拷贝，且电池控制***22确定电池21处于异 常状态时，为了保护电池受损，电池控制***22可控制电池21停止给无人机20供电。
所述当所述无人机的状态信息表示所述无人机处于非飞行状态，且所述电池处于异常状态时，控制所述电池停止给所述无人机供电，包括：当所述无人机的状态信息表示所述无人机处于非飞行状态，且所述电池欠压时，控制所述电池停止给所述无人机供电。
具体的，如果电池控制***22确定电池21的电压小于预设电压值，则电池控制***22确定电池21处于欠压状态。当电池控制***22确定出无人机20处于非飞行状态，例如无人机20在进行数据拷贝，且电池控制***22确定电池21处于欠压状态时，为了避免电池21在欠压状态下受损，电池控制***22可控制电池21停止给无人机20供电。
所述控制所述电池停止给所述无人机供电，包括：控制与所述电池连接的供电电路停止给所述无人机供电。
可选的，电池控制***22控制电池21停止给无人机20供电的一种可行的实现方式是：电池控制***22控制与电池21连接的供电电路24停止给无人机20供电。
所述控制与所述电池连接的供电电路停止给所述无人机供电，包括：控制与所述电池连接的供电电路的开关断开，以使所述供电电路停止给所述无人机供电。
当电池控制***22确定出无人机20处于飞行状态，且电池21处于欠压状态时，电池控制***22可通过控制开关25断开，以使供电电路24停止给无人机20供电。
另外，如图3所示的电池控制***33和如图2所示的电池控制***22的实现方式和具体原理均一致，此处不再赘述。
本实施例通过电池控制***获取无人机的状态信息，以及电池的电参数信息，根据所述电池的电参数信息，确定所述电池是否异常，当无人机处于飞行状态，且所述电池处于异常状态时，电池控制***控制所述电池继续给所述无人机供电，避免无人机在飞行过程中由于电池断电而坠落，保证了无人机的安全性。
本发明实施例提供一种电池控制方法。图4为本发明另一实施例提供的电池控制方法的流程图。如图4所示，在图1所示实施例的基础上，本实施例中的方法，还可以包括：
步骤S401、检测所述电池控制***中的处理器的状态信息。
如图5所示，电池控制***22包括处理器26和驱动电路27，其中，所述处理器包括微控制单元MCU。驱动电路27用于控制与电池21连接的供电电路24的开关25。
所述检测所述电池控制***中的处理器的状态信息，包括：所述电池控制***中的驱动电路检测所述电池控制***中的处理器是否异常，所述驱动电路用于控制与电池连接的供电电路的开关。
可选的，电池控制***22中的驱动电路27检测处理器26是否异常。
步骤S402、根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关。
具体的，驱动电路27可根据处理器26的状态信息，控制与电池21连接的供电电路24的开关25。
具体的，根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关，包括：若所述处理器处于异常状态，则所述驱动电路控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述无人机供电。
例如，当驱动电路27确定出处理器26处于异常状态时，驱动电路27可控制与电池21连接的供电电路24的开关25闭合，以使供电电路24继续给无人机20供电。
所述电池控制***中的驱动电路检测所述电池控制***中的处理器是否异常，包括：所述电池控制***中的驱动电路检测所述电池控制***中的处理器是否处于复位状态。
具体的，电池控制***22中的驱动电路27可检测处理器26是否处于复位状态。
所述若所述处理器处于异常状态，则所述驱动电路控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述无人机供电，包括：若所述处理器处于复位状态，则所述驱动电路控制与所述电池连接的 供电电路的开关闭合，以使所述供电电路继续给所述无人机供电。
例如，当驱动电路27确定出处理器26处于复位状态时，驱动电路27可控制与电池21连接的供电电路24的开关25闭合，以使供电电路24继续给无人机20供电，避免处理器26受到干扰复位时电池21立即停止给无人机20供电而导致飞行状态的无人机20被迫炸机。在其他实施例中，当处理器26受到干扰复位时，飞行控制器23可能无法与处理器26进行正常通讯，此时，飞行控制器23可以控制无人机20下降而避免炸机。
另外，所述根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关，包括：当所述处理器处于升级状态，且所述电池的电流大于或等于电流阈值时，控制与所述电池连接的供电电路的开关断开，以使所述供电电路停止供电。
具体的，处理器26还可以检测其状态信息，例如，处理器26还可以检测其是否处于升级状态，当处理器26处于升级状态时，升级loader还可以检测电池21的电压和/或电流，进一步的，处理器26还可以根据电池21的电压和/或电流，控制与电池21连接的供电电路24的开关25。
例如，当处理器26处于升级状态，且电池21的电流大于或等于电流阈值即过流时，处理器26控制与电池21连接的供电电路24的开关25断开，以使供电电路24停止供电，避免电池21由于过流而损坏。
此外，所述根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关，包括：当所述处理器处于升级状态，且所述电池的电压小于或等于第一电压阈值时，控制与所述电池连接的供电电路的开关断开，以使所述供电电路停止供电。
例如，当处理器26处于升级状态，且电池21的电压小于或等于第一电压阈值即欠压时，处理器26控制与电池21连接的供电电路24的开关25断开，以使供电电路24停止供电，避免电池21由于欠压而损坏。可选的，该第一电压阈值为3.2V。
在其他实施例中，所述方法还包括如图6所示的如下步骤：
步骤S601、检测所述电池的状态信息。
如图5所示，处理器26还可以检测电池21的状态信息。例如，当电池21的电压小于或等于3.2V后，需要对电池21进行充电。处理器26具 体可以检测电池21是否处于充电状态。
可选的，当处理器26处于升级状态时，电池21向外供电；当电池21连接充电器时，电池21开始充电、不向外供电。在本实施例中，电池21不限于给无人机供电，还可以给其他负载供电。
步骤S602、当所述电池处于充电状态，且所述电池的电压大于或等于第二电压阈值时，控制与所述电池连接的供电电路的开关闭合，以使所述供电电路对外供电。
例如，当处理器26处于升级状态时，电池21向外供电，电池21的电压不断减小，当电池21的电压小于或等于例如3.2V时，处理器26控制与电池21连接的供电电路24的开关25断开，此时，电池21无法向外供电，避免电池21受损。
当电池21处于充电状态时，电池21的电压不断增大，当电池21的电压大于或等于第二电压阈值例如3.8V时，处理器26控制与电池21连接的供电电路24的开关25闭合，此时，电池21可以向外供电。
步骤S603、当所述电池处于充电状态，且所述电池的电压大于或等于第三电压阈值时，控制与所述电池连接的充电电路的开关断开，以使所述充电电路停止给所述电池充电。
当电池21处于充电状态时，电池21的电压不断增大，当电池21的电压大于或等于第二电压阈值例如3.8V时，处理器26控制与电池21连接的供电电路24的开关25闭合，此时，电池21可以向外供电。如果此时，电池21继续充电，则电池21的电压将继续增大，当电池21的电压大于或等于第三电压阈值例如4.2V即电池21过压时，处理器26还可以控制与电池21连接的充电电路的开关断开。由于该电池21通过该充电电路与充电器连接，当处理器26控制与电池21连接的充电电路的开关断开时，相当于控制电池21与充电器之间的连接断开，使得充电器停止给电池21继续充电，从而避免电池21在充电过程中电压过高或温度过高而影响电池21的性能。
本实施例通过检测所述电池控制***中的处理器的状态信息，根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关，避免处理器受到干扰复位时电池立即停止给无人机供电而导致飞行状态的无人机 被迫炸机；另外，当处理器处于升级状态，且电池欠压或过流时，处理器控制与电池连接的供电电路的开关断开，以使供电电路停止供电，避免电池由于欠压或过流而损坏，在保证无人机安全飞行的基础上，还可避免电池受损。此外，通过电池在充电过程中，对电池的电压进行检测，当电池过压时，控制与电池连接的充电电路的开关断开，以使充电电路停止给电池充电，避免电池过压而损坏。
本发明实施例提供一种电池控制方法。图7为本发明另一实施例提供的电池控制方法的流程图。如图7所示，本实施例所述的电池控制方法应用于电池控制***，本实施例中的方法，可以包括：
步骤S701、检测所述电池控制***中的处理器的状态信息。
如图5所示，电池控制***22包括处理器26和驱动电路27，其中，所述处理器包括微控制单元MCU。驱动电路27用于控制与电池21连接的供电电路24的开关25。
所述检测所述电池控制***中的处理器的状态信息，包括：所述电池控制***中的驱动电路检测所述电池控制***中的处理器是否异常，所述驱动电路用于控制与电池连接的供电电路的开关。
可选的，电池控制***22中的驱动电路27检测处理器26是否异常。
步骤S702、根据所述处理器的状态信息，控制与电池连接的供电电路的开关，所述电池用于给可移动平台供电。
具体的，驱动电路27可根据处理器26的状态信息，控制与电池21连接的供电电路24的开关25，电池21用于给可移动平台供电，可选的，所述可移动平台包括无人机。
所述根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关，包括：若所述处理器处于异常状态，则所述驱动电路控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述可移动平台供电。
例如，当驱动电路27确定出处理器26处于异常状态时，驱动电路27可控制与电池21连接的供电电路24的开关25闭合，以使供电电路24继续给无人机20供电。
所述电池控制***中的驱动电路检测所述电池控制***中的处理器是否异常，包括：所述电池控制***中的驱动电路检测所述电池控制***中的处理器是否处于复位状态。
具体的，电池控制***22中的驱动电路27可检测处理器26是否处于复位状态。
所述若所述处理器处于异常状态，则所述驱动电路控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述可移动平台供电，包括：若所述处理器处于复位状态，则所述驱动电路控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述可移动平台供电。
例如，当驱动电路27确定出处理器26处于复位状态时，驱动电路27可控制与电池21连接的供电电路24的开关25闭合，以使供电电路24继续给无人机20供电，避免处理器26受到干扰复位时电池21立即停止给无人机20供电而导致飞行状态的无人机20被迫炸机。在其他实施例中，当处理器26受到干扰复位时，飞行控制器23可能无法与处理器26进行正常通讯，此时，飞行控制器23可以控制无人机20下降而避免炸机。
另外，所述根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关，包括：当所述处理器处于升级状态，且所述电池的电流大于或等于电流阈值时，控制与所述电池连接的供电电路的开关断开，以使所述供电电路停止供电。
具体的，处理器26还可以检测其状态信息，例如，处理器26还可以检测其是否处于升级状态，当处理器26处于升级状态时，升级loader还可以检测电池21的电压和/或电流，进一步的，处理器26还可以根据电池21的电压和/或电流，控制与电池21连接的供电电路24的开关25。
例如，当处理器26处于升级状态，且电池21的电流大于或等于电流阈值即过流时，处理器26控制与电池21连接的供电电路24的开关25断开，以使供电电路24停止供电，避免电池21由于过流而损坏。
此外，所述根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关，包括：当所述处理器处于升级状态，且所述电池的电压小于或等于第一电压阈值时，控制与所述电池连接的供电电路的开关断开，以使所述供电电路停止供电。
例如，当处理器26处于升级状态，且电池21的电压小于或等于第一电压阈值即欠压时，处理器26控制与电池21连接的供电电路24的开关25断开，以使供电电路24停止供电，避免电池21由于欠压而损坏。可选的，该第一电压阈值为3.2V。
本实施例通过检测所述电池控制***中的处理器的状态信息，根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关，避免处理器受到干扰复位时电池立即停止给无人机供电而导致飞行状态的无人机被迫炸机；另外，当处理器处于升级状态，且电池欠压或过流时，处理器控制与电池连接的供电电路的开关断开，以使供电电路停止供电，避免电池由于欠压或过流而损坏，在保证无人机安全飞行的基础上，还可避免电池受损。
本发明实施例提供一种电池控制***。图8为本发明实施例提供的电池控制***的结构图，如图8所示，电池控制***80包括一个或多个处理器81。处理器81用于：获取无人机的状态信息，以及电池的电参数信息，所述电池用于给所述无人机供电；根据所述电池的电参数信息，确定所述电池是否异常；当所述无人机的状态信息表示所述无人机处于飞行状态，且所述电池处于异常状态时，控制所述电池继续给所述无人机供电。
可选的，所述电池的电参数信息包括如下至少一种：所述电池的电压、电流、输出功率、剩余电量、温度。
可选的，处理器81根据所述电池的电参数信息，确定所述电池是否异常时，具体用于：根据所述电池的电压，确定所述电池是否欠压；当所述无人机的状态信息表示所述无人机处于飞行状态，且所述电池处于异常状态时，处理器81控制所述电池继续给所述无人机供电。
可选的，处理器81控制所述电池继续给所述无人机供电时，具体用于：控制与所述电池连接的供电电路继续给所述无人机供电。
可选的，处理器81控制与所述电池连接的供电电路继续给所述无人机供电时，具体用于：控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述无人机供电。
可选的，处理器81还用于：当所述无人机的状态信息表示所述无人 机处于非飞行状态，且所述电池处于异常状态时，控制所述电池停止给所述无人机供电。
可选的，当所述无人机的状态信息表示所述无人机处于非飞行状态，且所述电池欠压时处理器81控制所述电池停止给所述无人机供电。
可选的，处理器81控制所述电池停止给所述无人机供电时，具体用于：控制与所述电池连接的供电电路停止给所述无人机供电。
可选的，处理器81控制与所述电池连接的供电电路停止给所述无人机供电时，具体用于：控制与所述电池连接的供电电路的开关断开，以使所述供电电路停止给所述无人机供电。
可选的，处理器81获取无人机的状态信息时，具体用于：接收所述无人机的飞行控制器发送的所述无人机的状态信息。
可选的，电池控制***80还包括：驱动电路82，驱动电路82与处理器81电连接，驱动电路82用于：检测所述电池控制***中的处理器的状态信息；根据处理器81的状态信息，控制与所述电池连接的供电电路的开关。
可选的，驱动电路82检测所述电池控制***中的处理器的状态信息时，具体用于：驱动电路82检测所述电池控制***中的处理器是否异常；驱动电路82根据处理器81的状态信息，控制与所述电池连接的供电电路的开关时，具体用于：若处理器81处于异常状态，则驱动电路82控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述无人机供电处理器81。
可选的，驱动电路82检测所述电池控制***中的处理器是否异常时，具体用于：检测所述电池控制***中的处理器是否处于复位状态；若处理器81处于复位状态，则驱动电路82控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述无人机供电。
可选的，处理器81还用于：检测处理器81的状态信息；根据处理器81的状态信息，控制与所述电池连接的供电电路的开关。
可选的，处理器81根据处理器81的状态信息，控制与所述电池连接的供电电路的开关时，具体用于：当处理器81处于升级状态，且所述电池的电流大于或等于电流阈值时，控制与所述电池连接的供电电路的开关 断开，以使所述供电电路停止供电。
可选的，处理器81根据处理器81的状态信息，控制与所述电池连接的供电电路的开关时，具体用于：当处理器81处于升级状态，且所述电池的电压小于或等于第一电压阈值时，控制与所述电池连接的供电电路的开关断开，以使所述供电电路停止供电。
可选的，处理器81还用于：检测所述电池的状态信息；当所述电池处于充电状态，且所述电池的电压大于或等于第二电压阈值时，控制与所述电池连接的供电电路的开关闭合，以使所述供电电路对外供电。
可选的，处理器81还用于：当所述电池处于充电状态，且所述电池的电压大于或等于第三电压阈值时，控制与所述电池连接的充电电路的开关断开，以使所述充电电路停止给所述电池充电。
可选的，处理器81包括微控制单元MCU。
本发明实施例提供的电池控制***的具体原理和实现方式均与图1、图4或图6所示实施例类似，此处不再赘述。
本实施例通过电池控制***获取无人机的状态信息，以及电池的电参数信息，根据所述电池的电参数信息，确定所述电池是否异常，当无人机处于飞行状态，且所述电池处于异常状态时，电池控制***控制所述电池继续给所述无人机供电，避免无人机在飞行过程中由于电池断电而坠落，保证了无人机的安全性。
本发明实施例提供一种电池控制***。如图8所示，电池控制***80包括一个或多个处理器81，处理器81用于：检测处理器81的状态信息；根据处理器81的状态信息，控制与电池连接的供电电路的开关，所述电池用于给可移动平台供电。
可选的，处理器81根据处理器81的状态信息，控制与电池连接的供电电路的开关时，具体用于：当处理器81处于升级状态，且所述电池的电流大于或等于电流阈值时，控制与所述电池连接的供电电路的开关断开，以使所述供电电路停止供电。
可选的，处理器81根据处理器81的状态信息，控制与电池连接的供电电路的开关时，具体用于：当处理器81处于升级状态，且所述电池的 电压小于或等于第一电压阈值时，控制与所述电池连接的供电电路的开关断开，以使所述供电电路停止供电。
可选的，所述可移动平台包括无人机。
本发明实施例提供的电池控制***的具体原理和实现方式均与图7所示实施例类似，此处不再赘述。
本实施例通过检测所述电池控制***中的处理器的状态信息，根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关，避免处理器受到干扰复位时电池立即停止给无人机供电而导致飞行状态的无人机被迫炸机；另外，当处理器处于升级状态，且电池欠压或过流时，处理器控制与电池连接的供电电路的开关断开，以使供电电路停止供电，避免电池由于欠压或过流而损坏，在保证无人机安全飞行的基础上，还可避免电池受损。
本发明实施例提供一种电池控制***。如图8所示，电池控制***80包括一个或多个处理器81和驱动电路82，处理器81和驱动电路82电连接，驱动电路82用于控制与电池连接的供电电路的开关，所述电池用于给可移动平台供电；处理器81用于通过驱动电路82控制所述开关；驱动电路82用于：检测所述电池控制***中的处理器的状态信息；根据处理器81的状态信息，控制与电池连接的供电电路的开关。
可选的，驱动电路82检测所述电池控制***中的处理器的状态信息时，具体用于：检测所述电池控制***中的处理器是否异常；驱动电路82根据处理器81的状态信息，控制与电池连接的供电电路的开关时，具体用于：若处理器81处于异常状态，则驱动电路82控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述可移动平台供电。
可选的，驱动电路82检测所述电池控制***中的处理器是否异常时，具体用于：检测所述电池控制***中的处理器是否处于复位状态；若处理器81处于复位状态，则驱动电路82控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述可移动平台供电。
可选的，所述可移动平台包括无人机。
本发明实施例提供的电池控制***的具体原理和实现方式均与图7所 示实施例类似，此处不再赘述。
本实施例通过检测所述电池控制***中的处理器的状态信息，根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关，避免处理器受到干扰复位时电池立即停止给无人机供电而导致飞行状态的无人机被迫炸机；另外，当处理器处于升级状态，且电池欠压或过流时，处理器控制与电池连接的供电电路的开关断开，以使供电电路停止供电，避免电池由于欠压或过流而损坏，在保证无人机安全飞行的基础上，还可避免电池受损。
本发明实施例提供一种无人机。图9为本发明实施例提供的无人机的结构图，如图9所示，无人机900包括：机身、动力***、飞行控制器918和电池控制***919，所述动力***包括如下至少一种：电机907、螺旋桨906和电子调速器917，动力***安装在所述机身，用于提供飞行动力；飞行控制器918与所述动力***通讯连接，用于控制所述无人机飞行。
电池控制***919的具体原理和实现方式均与上述实施例类似，此处不再赘述。
另外，如图9所示，无人机900还包括：支撑设备902、拍摄设备904，其中，支撑设备902具体可以是云台。
本实施例通过电池控制***获取无人机的状态信息，以及电池的电参数信息，根据所述电池的电参数信息，确定所述电池是否异常，当无人机处于飞行状态，且所述电池处于异常状态时，电池控制***控制所述电池继续给所述无人机供电，避免无人机在飞行过程中由于电池断电而坠落，保证了无人机的安全性。
本发明实施例提供一种电池。图10为本发明实施例提供的电池的结构图，如图10所示，电池1000包括：壳体1001、电芯1002、电池控制***1003。其中，电芯1002安装在壳体1001内，电池控制***1003安装在壳体1001内，电池控制***1003和电芯1002电连接。电池控制***1003的具体原理和实现方式均与上述实施例类似，此处不再赘述。
本实施例通过电池控制***获取无人机的状态信息，以及电池的电参 数信息，根据所述电池的电参数信息，确定所述电池是否异常，当无人机处于飞行状态，且所述电池处于异常状态时，电池控制***控制所述电池继续给所述无人机供电，避免无人机在飞行过程中由于电池断电而坠落，保证了无人机的安全性。
在本发明所提供的几个实施例中，应该理解到，所揭露的装置和方法，可以通过其它的方式实现。例如，以上所描述的装置实施例仅仅是示意性的，例如，所述单元的划分，仅仅为一种逻辑功能划分，实际实现时可以有另外的划分方式，例如多个单元或组件可以结合或者可以集成到另一个***，或一些特征可以忽略，或不执行。另一点，所显示或讨论的相互之间的耦合或直接耦合或通信连接可以是通过一些接口，装置或单元的间接耦合或通信连接，可以是电性，机械或其它的形式。
所述作为分离部件说明的单元可以是或者也可以不是物理上分开的，作为单元显示的部件可以是或者也可以不是物理单元，即可以位于一个地方，或者也可以分布到多个网络单元上。可以根据实际的需要选择其中的部分或者全部单元来实现本实施例方案的目的。
另外，在本发明各个实施例中的各功能单元可以集成在一个处理单元中，也可以是各个单元单独物理存在，也可以两个或两个以上单元集成在一个单元中。上述集成的单元既可以采用硬件的形式实现，也可以采用硬件加软件功能单元的形式实现。
上述以软件功能单元的形式实现的集成的单元，可以存储在一个计算机可读取存储介质中。上述软件功能单元存储在一个存储介质中，包括若干指令用以使得一台计算机设备(可以是个人计算机，服务器，或者网络设备等)或处理器(processor)执行本发明各个实施例所述方法的部分步骤。而前述的存储介质包括：U盘、移动硬盘、只读存储器(Read-Only Memory，ROM)、随机存取存储器(Random Access Memory，RAM)、磁碟或者光盘等各种可以存储程序代码的介质。
本领域技术人员可以清楚地了解到，为描述的方便和简洁，仅以上述各功能模块的划分进行举例说明，实际应用中，可以根据需要而将上述功能分配由不同的功能模块完成，即将装置的内部结构划分成不同的功能模 块，以完成以上描述的全部或者部分功能。上述描述的装置的具体工作过程，可以参考前述方法实施例中的对应过程，在此不再赘述。
最后应说明的是：以上各实施例仅用以说明本发明的技术方案，而非对其限制；尽管参照前述各实施例对本发明进行了详细的说明，本领域的普通技术人员应当理解：其依然可以对前述各实施例所记载的技术方案进行修改，或者对其中部分或者全部技术特征进行等同替换；而这些修改或者替换，并不使相应技术方案的本质脱离本发明各实施例技术方案的范围。

Claims (53)

  1. 一种电池控制方法，应用于电池控制***，其特征在于，包括：
    获取无人机的状态信息，以及电池的电参数信息，其中，所述电池用于给所述无人机供电；
    根据所述电池的电参数信息，确定所述电池是否异常；
    当所述无人机的状态信息表示所述无人机处于飞行状态，且所述电池处于异常状态时，控制所述电池继续给所述无人机供电。
  2. 根据权利要求1所述的方法，其特征在于，所述电池的电参数信息包括如下至少一种：
    所述电池的电压、电流、输出功率、剩余电量、温度。
  3. 根据权利要求2所述的方法，其特征在于，所述根据所述电池的电参数信息，确定所述电池是否异常，包括：
    根据所述电池的电压，确定所述电池是否欠压；
    所述当所述无人机的状态信息表示所述无人机处于飞行状态，且所述电池处于异常状态时，控制所述电池继续给所述无人机供电，包括：
    当所述无人机的状态信息表示所述无人机处于飞行状态，且所述电池欠压时，控制所述电池继续给所述无人机供电。
  4. 根据权利要求1-3任一项所述的方法，其特征在于，所述控制所述电池继续给所述无人机供电，包括：
    控制与所述电池连接的供电电路继续给所述无人机供电。
  5. 根据权利要求4所述的方法，其特征在于，所述控制与所述电池连接的供电电路继续给所述无人机供电，包括：
    控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述无人机供电。
  6. 根据权利要求1-3任一项所述的方法，其特征在于，所述方法还包括：
    当所述无人机的状态信息表示所述无人机处于非飞行状态，且所述电池处于异常状态时，控制所述电池停止给所述无人机供电。
  7. 根据权利要求6所述的方法，其特征在于，所述当所述无人机的状态信息表示所述无人机处于非飞行状态，且所述电池处于异常状态时， 控制所述电池停止给所述无人机供电，包括：
    当所述无人机的状态信息表示所述无人机处于非飞行状态，且所述电池欠压时，控制所述电池停止给所述无人机供电。
  8. 根据权利要求6或7所述的方法，其特征在于，所述控制所述电池停止给所述无人机供电，包括：
    控制与所述电池连接的供电电路停止给所述无人机供电。
  9. 根据权利要求8所述的方法，其特征在于，所述控制与所述电池连接的供电电路停止给所述无人机供电，包括：
    控制与所述电池连接的供电电路的开关断开，以使所述供电电路停止给所述无人机供电。
  10. 根据权利要求1-9任一项所述的方法，其特征在于，所述获取无人机的状态信息，包括：
    接收所述无人机的飞行控制器发送的所述无人机的状态信息。
  11. 根据权利要求1所述的方法，其特征在于，所述方法还包括：
    检测所述电池控制***中的处理器的状态信息；
    根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关。
  12. 根据权利要求11所述的方法，其特征在于，所述检测所述电池控制***中的处理器的状态信息，包括：
    所述电池控制***中的驱动电路检测所述电池控制***中的处理器是否异常，所述驱动电路用于控制与电池连接的供电电路的开关；
    所述根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关，包括：
    若所述处理器处于异常状态，则所述驱动电路控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述无人机供电。
  13. 根据权利要求12所述的方法，其特征在于，所述电池控制***中的驱动电路检测所述电池控制***中的处理器是否异常，包括：
    所述电池控制***中的驱动电路检测所述电池控制***中的处理器是否处于复位状态；
    所述若所述处理器处于异常状态，则所述驱动电路控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述无人机供电，包 括：
    若所述处理器处于复位状态，则所述驱动电路控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述无人机供电。
  14. 根据权利要求11所述的方法，其特征在于，所述根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关，包括：
    当所述处理器处于升级状态，且所述电池的电流大于或等于电流阈值时，控制与所述电池连接的供电电路的开关断开，以使所述供电电路停止供电。
  15. 根据权利要求11所述的方法，其特征在于，所述根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关，包括：
    当所述处理器处于升级状态，且所述电池的电压小于或等于第一电压阈值时，控制与所述电池连接的供电电路的开关断开，以使所述供电电路停止供电。
  16. 根据权利要求1所述的方法，其特征在于，所述方法还包括：
    检测所述电池的状态信息；
    当所述电池处于充电状态，且所述电池的电压大于或等于第二电压阈值时，控制与所述电池连接的供电电路的开关闭合，以使所述供电电路对外供电。
  17. 根据权利要求16所述的方法，其特征在于，所述方法还包括：
    当所述电池处于充电状态，且所述电池的电压大于或等于第三电压阈值时，控制与所述电池连接的充电电路的开关断开，以使所述充电电路停止给所述电池充电。
  18. 根据权利要求11-15任一项所述的方法，其特征在于，所述处理器包括微控制单元MCU。
  19. 一种电池控制方法，应用于电池控制***，其特征在于，包括：
    检测所述电池控制***中的处理器的状态信息；
    根据所述处理器的状态信息，控制与电池连接的供电电路的开关，所述电池用于给可移动平台供电。
  20. 根据权利要求19所述的方法，其特征在于，所述检测所述电池控制***中的处理器的状态信息，包括：
    所述电池控制***中的驱动电路检测所述电池控制***中的处理器是否异常，所述驱动电路用于控制与电池连接的供电电路的开关；
    所述根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关，包括：
    若所述处理器处于异常状态，则所述驱动电路控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述可移动平台供电。
  21. 根据权利要求20所述的方法，其特征在于，所述电池控制***中的驱动电路检测所述电池控制***中的处理器是否异常，包括：
    所述电池控制***中的驱动电路检测所述电池控制***中的处理器是否处于复位状态；
    所述若所述处理器处于异常状态，则所述驱动电路控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述可移动平台供电，包括：
    若所述处理器处于复位状态，则所述驱动电路控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述可移动平台供电。
  22. 根据权利要求19所述的方法，其特征在于，所述根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关，包括：
    当所述处理器处于升级状态，且所述电池的电流大于或等于电流阈值时，控制与所述电池连接的供电电路的开关断开，以使所述供电电路停止供电。
  23. 根据权利要求19所述的方法，其特征在于，所述根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关，包括：
    当所述处理器处于升级状态，且所述电池的电压小于或等于第一电压阈值时，控制与所述电池连接的供电电路的开关断开，以使所述供电电路停止供电。
  24. 根据权利要求19-23任一项所述的方法，其特征在于，所述可移动平台包括无人机。
  25. 一种电池控制***，其特征在于，所述电池控制***包括：
    一个或多个处理器，所述处理器用于：
    获取无人机的状态信息，以及电池的电参数信息，所述电池用于给所 述无人机供电；
    根据所述电池的电参数信息，确定所述电池是否异常；
    当所述无人机的状态信息表示所述无人机处于飞行状态，且所述电池处于异常状态时，控制所述电池继续给所述无人机供电。
  26. 根据权利要求25所述的电池控制***，其特征在于，所述电池的电参数信息包括如下至少一种：
    所述电池的电压、电流、输出功率、剩余电量、温度。
  27. 根据权利要求26所述的电池控制***，其特征在于，所述处理器根据所述电池的电参数信息，确定所述电池是否异常时，具体用于：
    根据所述电池的电压，确定所述电池是否欠压；
    当所述无人机的状态信息表示所述无人机处于飞行状态，且所述电池处于异常状态时，所述处理器控制所述电池继续给所述无人机供电。
  28. 根据权利要求25-27任一项所述的电池控制***，其特征在于，所述处理器控制所述电池继续给所述无人机供电时，具体用于：
    控制与所述电池连接的供电电路继续给所述无人机供电。
  29. 根据权利要求28所述的电池控制***，其特征在于，所述处理器控制与所述电池连接的供电电路继续给所述无人机供电时，具体用于：
    控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述无人机供电。
  30. 根据权利要求25-27任一项所述的电池控制***，其特征在于，所述处理器还用于：
    当所述无人机的状态信息表示所述无人机处于非飞行状态，且所述电池处于异常状态时，控制所述电池停止给所述无人机供电。
  31. 根据权利要求30所述的电池控制***，其特征在于，当所述无人机的状态信息表示所述无人机处于非飞行状态，且所述电池欠压时所述处理器控制所述电池停止给所述无人机供电。
  32. 根据权利要求30或31所述的电池控制***，其特征在于，所述处理器控制所述电池停止给所述无人机供电时，具体用于：
    控制与所述电池连接的供电电路停止给所述无人机供电。
  33. 根据权利要求32所述的电池控制***，其特征在于，所述处理 器控制与所述电池连接的供电电路停止给所述无人机供电时，具体用于：
    控制与所述电池连接的供电电路的开关断开，以使所述供电电路停止给所述无人机供电。
  34. 根据权利要求25-33任一项所述的电池控制***，其特征在于，所述处理器获取无人机的状态信息时，具体用于：
    接收所述无人机的飞行控制器发送的所述无人机的状态信息。
  35. 根据权利要求25所述的电池控制***，其特征在于，还包括：
    驱动电路，与所述处理器电连接，所述驱动电路用于：
    检测所述电池控制***中的处理器的状态信息；
    根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关。
  36. 根据权利要求35所述的电池控制***，其特征在于，所述驱动电路检测所述电池控制***中的处理器的状态信息时，具体用于：
    所述驱动电路检测所述电池控制***中的处理器是否异常；
    所述驱动电路根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关时，具体用于：
    若所述处理器处于异常状态，则所述驱动电路控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述无人机供电。
  37. 根据权利要求36所述的电池控制***，其特征在于，所述驱动电路检测所述电池控制***中的处理器是否异常时，具体用于：检测所述电池控制***中的处理器是否处于复位状态；
    若所述处理器处于复位状态，则所述驱动电路控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述无人机供电。
  38. 根据权利要求25所述的电池控制***，其特征在于，所述处理器还用于：
    检测所述处理器的状态信息；
    根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关。
  39. 根据权利要求38所述的电池控制***，其特征在于，所述处理器根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关时，具体用于：
    当所述处理器处于升级状态，且所述电池的电流大于或等于电流阈值 时，控制与所述电池连接的供电电路的开关断开，以使所述供电电路停止供电。
  40. 根据权利要求38所述的电池控制***，其特征在于，所述处理器根据所述处理器的状态信息，控制与所述电池连接的供电电路的开关时，具体用于：
    当所述处理器处于升级状态，且所述电池的电压小于或等于第一电压阈值时，控制与所述电池连接的供电电路的开关断开，以使所述供电电路停止供电。
  41. 根据权利要求25所述的电池控制***，其特征在于，所述处理器还用于：
    检测所述电池的状态信息；
    当所述电池处于充电状态，且所述电池的电压大于或等于第二电压阈值时，控制与所述电池连接的供电电路的开关闭合，以使所述供电电路对外供电。
  42. 根据权利要求41所述的电池控制***，其特征在于，所述处理器还用于：
    当所述电池处于充电状态，且所述电池的电压大于或等于第三电压阈值时，控制与所述电池连接的充电电路的开关断开，以使所述充电电路停止给所述电池充电。
  43. 根据权利要求25-42任一项所述的电池控制***，其特征在于，所述处理器包括微控制单元MCU。
  44. 一种电池控制***，其特征在于，包括：
    一个或多个处理器，所述处理器用于：
    检测所述处理器的状态信息；
    根据所述处理器的状态信息，控制与电池连接的供电电路的开关，所述电池用于给可移动平台供电。
  45. 根据权利要求44所述的电池控制***，其特征在于，所述处理器根据所述处理器的状态信息，控制与电池连接的供电电路的开关时，具体用于：
    当所述处理器处于升级状态，且所述电池的电流大于或等于电流阈值 时，控制与所述电池连接的供电电路的开关断开，以使所述供电电路停止供电。
  46. 根据权利要求44所述的电池控制***，其特征在于，所述处理器根据所述处理器的状态信息，控制与电池连接的供电电路的开关时，具体用于：
    当所述处理器处于升级状态，且所述电池的电压小于或等于第一电压阈值时，控制与所述电池连接的供电电路的开关断开，以使所述供电电路停止供电。
  47. 根据权利要求44-46任一项所述的电池控制***，其特征在于，所述可移动平台包括无人机。
  48. 一种电池控制***，其特征在于，包括：
    驱动电路，所述驱动电路用于控制与电池连接的供电电路的开关，所述电池用于给可移动平台供电；
    一个或多个处理器，所述处理器与所述驱动电路电连接，用于通过所述驱动电路控制所述开关；
    所述驱动电路用于：
    检测所述电池控制***中的处理器的状态信息；
    根据所述处理器的状态信息，控制与电池连接的供电电路的开关。
  49. 根据权利要求48所述的电池控制***，其特征在于，所述驱动电路检测所述电池控制***中的处理器的状态信息时，具体用于：
    检测所述电池控制***中的处理器是否异常；
    所述驱动电路根据所述处理器的状态信息，控制与电池连接的供电电路的开关时，具体用于：
    若所述处理器处于异常状态，则所述驱动电路控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述可移动平台供电。
  50. 根据权利要求49所述的电池控制***，其特征在于，所述驱动电路检测所述电池控制***中的处理器是否异常时，具体用于：检测所述电池控制***中的处理器是否处于复位状态；
    若所述处理器处于复位状态，则所述驱动电路控制与所述电池连接的供电电路的开关闭合，以使所述供电电路继续给所述可移动平台供电。
  51. 根据权利要求48-50任一项所述的电池控制***，其特征在于，所述可移动平台包括无人机。
  52. 一种无人机，其特征在于，包括：
    机身；
    动力***，安装在所述机身，用于提供飞行动力；
    飞行控制器，与所述动力***通讯连接，用于控制所述无人机飞行；以及
    如权利要求25-51任一项所述的电池控制***。
  53. 一种电池，其特征在于，包括：
    壳体；
    电芯，安装在所述壳体内；以及
    权利要求25-51任一项所述的电池控制***，安装在所述壳体内；
    其中，所述电池控制***与所述电芯电连接。
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