CN108490964A - Control method, device and the intelligent terminal of unmanned plane - Google Patents
Control method, device and the intelligent terminal of unmanned plane Download PDFInfo
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- CN108490964A CN108490964A CN201810239165.2A CN201810239165A CN108490964A CN 108490964 A CN108490964 A CN 108490964A CN 201810239165 A CN201810239165 A CN 201810239165A CN 108490964 A CN108490964 A CN 108490964A
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- 238000000034 method Methods 0.000 title claims abstract description 51
- 230000005059 dormancy Effects 0.000 claims abstract description 20
- 230000007958 sleep Effects 0.000 claims abstract description 19
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims description 13
- 230000005540 biological transmission Effects 0.000 claims description 4
- 238000004891 communication Methods 0.000 claims description 4
- 238000001514 detection method Methods 0.000 claims description 4
- 230000002618 waking effect Effects 0.000 claims description 2
- 230000006870 function Effects 0.000 description 16
- 238000010586 diagram Methods 0.000 description 15
- 238000012360 testing method Methods 0.000 description 5
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- 238000005516 engineering process Methods 0.000 description 4
- 230000008859 change Effects 0.000 description 2
- 238000013461 design Methods 0.000 description 2
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- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 235000008434 ginseng Nutrition 0.000 description 1
- 230000006266 hibernation Effects 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
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- 230000035484 reaction time Effects 0.000 description 1
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Classifications
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
- G01D21/00—Measuring or testing not otherwise provided for
- G01D21/02—Measuring two or more variables by means not covered by a single other subclass
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0011—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0011—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement
- G05D1/0016—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement characterised by the operator's input device
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- Automation & Control Theory (AREA)
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Abstract
The present invention provides a kind of control method of unmanned plane, device and intelligent terminals, are related to unmanned aerial vehicle (UAV) control technical field, and this method includes：When the control system of intelligent terminal and unmanned plane is in connection status, the status information of unmanned plane is obtained；When status information is lock state information, key dormancy instruction input by user is received；Sleep command is sent to the connection equipment between the control system or control system and intelligent terminal of unmanned plane, so that control system or connection equipment enter dormant state；When receiving key wake-up instruction input by user, wake-up command is sent to control system or connection equipment, so that control system or connection equipment exit dormant state.Control method, device and the intelligent terminal of unmanned plane provided in an embodiment of the present invention, the function that the key of a key suspend mode unmanned plane/mono- wakes up unmanned plane is increased at intelligent terminal, unmanned plane can not unlock in the dormant state, unexpected caused by dangerous unlock to reduce.
Description
Technical field
The present invention relates to unmanned aerial vehicle (UAV) control technical fields, more particularly, to a kind of control method of unmanned plane, device and intelligence
It can terminal.
Background technology
With popularizing for unmanned plane (alternatively referred to as aircraft, aircraft), also got over therewith using the quantity of the user of unmanned plane
Come more, and since the degree of awareness that user operates unmanned plane is different, being easy to happen maloperation causes unmanned plane to unlock and send out
Outside business.For example, the user for being unfamiliar with unmanned plane completely may insecurely unlock unmanned plane simultaneously in the case of unmanned guidance
It takes off and causes accident, unmanned plane, user and other people safety are unable to get guarantee.
For can not effectively prevent problem unexpected caused by unmanned plane maloperation unlock in the prior art, not yet carry at present
Go out effective solution scheme.
Invention content
It, can be in view of this, the purpose of the present invention is to provide a kind of control method of unmanned plane, device and intelligent terminal
One key suspend mode wakes up unmanned plane, reduces the accident of dangerous unlock.
In a first aspect, an embodiment of the present invention provides a kind of control method of unmanned plane, it is applied to the intelligence of control unmanned plane
Energy terminal, including：When the control system of intelligent terminal and unmanned plane is in connection status, the status information of unmanned plane is obtained；
When status information is lock state information, key dormancy instruction input by user is received；Control system to unmanned plane or control
Connection equipment between system processed and intelligent terminal sends sleep command, so that control system or connection equipment enter suspend mode shape
State；In the dormant state, unmanned plane can not unlock；When receiving a key input by user and waking up instruction, to control system or
It connects equipment and sends wake-up command, so that control system or connection equipment exit dormant state.
With reference to first aspect, an embodiment of the present invention provides the first possible embodiments of first aspect, wherein control
System processed includes the flight control system or electron speed regulator of unmanned plane；It includes base station or day dead end to connect equipment.
With reference to first aspect, an embodiment of the present invention provides second of possible embodiments of first aspect, wherein
Before the step of obtaining the status information of unmanned plane, further include：Receive suspend mode account information input by user；According to suspend mode account
Information is logged in, and the control system for connecting intelligent terminal and unmanned plane is authenticated.
With reference to first aspect, an embodiment of the present invention provides the third possible embodiments of first aspect, wherein
Send wake-up command to control system or connection equipment so that control system or connection equipment the step of exiting dormant state it
Before, further include：It is logged in by the account for suspend mode.
With reference to first aspect, an embodiment of the present invention provides the 4th kind of possible embodiments of first aspect, wherein intelligence
Energy terminal is provided with a key suspend mode button；This method further includes：When status information is non-locking state information, by a key suspend mode
Button is set as invalid.
With reference to first aspect, an embodiment of the present invention provides the 5th kind of possible embodiment of first aspect, further include：
When control system or connection equipment in a dormant state when, in the self-detection result of output add dormant state prompt.
Second aspect, the embodiment of the present invention additionally provide a kind of control device of unmanned plane, are applied to control unmanned plane
Intelligent terminal, including：State information acquisition module, for being in connection status when the control system of intelligent terminal and unmanned plane
When, obtain the status information of unmanned plane；Command reception module, for when status information is lock state information, receiving user
One key dormancy instruction of input；Sleep block, between the control system or control system and intelligent terminal of unmanned plane
It connects equipment and sends sleep command, so that control system or connection equipment enter dormant state；In the dormant state, unmanned plane
It can not unlock；Wake-up module, for when receiving key wake-up instruction input by user, being sent out to control system or connection equipment
Wake-up command is sent, so that control system or connection equipment exit dormant state.
In conjunction with second aspect, an embodiment of the present invention provides the first possible embodiments of second aspect, wherein control
System processed includes the flight control system or electron speed regulator of unmanned plane；It includes base station or day dead end to connect equipment.
The third aspect, the embodiment of the present invention additionally provide a kind of intelligent terminal, including processor, memory, bus and logical
Believe interface, processor, communication interface and memory are connected by bus；Memory is for storing program；Processor, for passing through
Bus calls program stored in memory, executes the side of one of above-mentioned first aspect and its each possible embodiment offer
Method.
Fourth aspect, the embodiment of the present invention additionally provide a kind of non-volatile program code that can perform with processor
Computer-readable medium, program code make processor execute the offer of one of above-mentioned first aspect and its each possible embodiment
Method.
The embodiment of the present invention brings following advantageous effect：
Control method, device and the intelligent terminal of unmanned plane provided in an embodiment of the present invention, increase at intelligent terminal
The key of one key suspend mode unmanned plane/mono- wakes up the function of unmanned plane, and when unmanned plane is in the lock state, intelligent terminal can receive use
One key dormancy instruction of family input, and sent out to the connection equipment between the control system or control system and intelligent terminal of unmanned plane
It serves and states sleep command, so that control system or connection equipment enter dormant state, under the dormant state, unmanned plane can not
Unlock, it is unexpected caused by dangerous unlock to reduce, additional safety guarantee is provided.
Other feature and advantage of the disclosure will illustrate in the following description, alternatively, Partial Feature and advantage can be with
Deduce from specification or unambiguously determine, or by implement the disclosure above-mentioned technology it can be learnt that.
To enable the above objects, features, and advantages of the disclosure to be clearer and more comprehensible, preferred embodiment cited below particularly, and coordinate
Appended attached drawing, is described in detail below.
Description of the drawings
It, below will be to specific in order to illustrate more clearly of the specific embodiment of the invention or technical solution in the prior art
Embodiment or attached drawing needed to be used in the description of the prior art are briefly described, it should be apparent that, in being described below
Attached drawing is some embodiments of the present invention, for those of ordinary skill in the art, before not making the creative labor
It puts, other drawings may also be obtained based on these drawings.
Fig. 1 is the schematic diagram of unmanned aerial vehicle control system provided in an embodiment of the present invention；
Fig. 2 is a kind of flow chart of the control method of unmanned plane provided in an embodiment of the present invention；
Fig. 3 is the flow chart of the control method of another unmanned plane provided in an embodiment of the present invention；
Fig. 4 is the flow chart of the control method of another unmanned plane provided in an embodiment of the present invention；
Fig. 5 is the flow chart of the control method of another unmanned plane provided in an embodiment of the present invention；
Fig. 6 is a kind of structure diagram of the control device of unmanned plane provided in an embodiment of the present invention；
Fig. 7 is the structure diagram of the control device of another unmanned plane provided in an embodiment of the present invention；
Fig. 8 is the structure diagram of the control device of another unmanned plane provided in an embodiment of the present invention；
Fig. 9 is the structure diagram of the control device of another unmanned plane provided in an embodiment of the present invention；
Figure 10 is the structure diagram of the control device of another unmanned plane provided in an embodiment of the present invention.
Specific implementation mode
In order to make the object, technical scheme and advantages of the embodiment of the invention clearer, below in conjunction with attached drawing to the present invention
Technical solution be clearly and completely described, it is clear that described embodiments are some of the embodiments of the present invention, rather than
Whole embodiments.Based on the embodiments of the present invention, those of ordinary skill in the art are not making creative work premise
Lower obtained every other embodiment, shall fall within the protection scope of the present invention.
Unexpected caused by unmanned plane is unlocked due to maloperation, the embodiment of the present invention can not effectively be prevented in currently available technology
Control method, device and the intelligent terminal of a kind of unmanned plane provided with a key suspend mode or can wake up unmanned plane, reduce dangerous
The accident of unlock.
After unmanned plane landing locks, the unlocking motion of maloperation can be avoided to lead to accident by a key suspend mode aircraft
Generation；The user for being unfamiliar with product can be given to provide safety guarantee, avoid client in the case of unmanned guidance insecurely
Unlock, which is taken off, causes accident；By after a key suspend mode aircraft can to avoid aircraft loss (do not waken up first after suspend mode, nobody
Machine can not unlock flight, other people cannot use).It describes in detail below to the embodiment of the present invention.
The schematic diagram of unmanned aerial vehicle control system shown in Figure 1, be shown intelligent terminal, base station, remote controler and
Unmanned plane.
Include flight control system, electron speed regulator and day dead end in unmanned plane, which may include
Gyroscope, accelerometer, earth induction, baroceptor, ultrasonic sensor, GPS module and control circuit can be stablized
Unmanned plane during flying posture, and can control that unmanned plane is autonomous or the control system of semi-autonomous flight；The electron speed regulator can basis
The rotating speed of given control signal control motor, the motor are the driving motor of the propeller of unmanned plane；This day dead end is installation
It is returned to ground surface end in the data-signal etc. of the R-T unit on unmanned plane, vision signal, winged control that Airborne Camera can be acquired,
Flight control signal is exported simultaneously to equipment such as winged controls.
The application (APP) of control unmanned plane can be installed in advance in intelligent terminal, base station is pre-set at designated position.
Before control unmanned plane is flown, first carry out unmanned plane, base station, the connection of intelligent terminal and remote controler and aircraft from
Inspection.Intelligent terminal and remote controler can be communicatively coupled by base station and unmanned plane, can also directly be led to unmanned plane
Letter connection.
Embodiment 1
An embodiment of the present invention provides a kind of control methods of unmanned plane, are applied to the intelligent terminal of control unmanned plane, should
Intelligent terminal can be the intelligent mobile terminals such as smart mobile phone, tablet computer, can also be specially to design for controlling nobody
The intelligent mobile terminal of machine.
The flow chart of the control method of unmanned plane shown in Figure 2, this method comprises the following steps：
Step S202 obtains the state of unmanned plane when the control system of intelligent terminal and unmanned plane is in connection status
Information.
Intelligent terminal is attached with unmanned plane in advance.It is in connection status in the control system of intelligent terminal and unmanned plane
In the case of, intelligent terminal obtains the status information of unmanned plane.The control system of above-mentioned unmanned plane can be the flight of unmanned plane
Control system or electron speed regulator.The status information can be the state of flight information, standby mode information, locking shape of unmanned plane
State information etc. indicates the different operating statuses that unmanned plane is in respectively.
Step S204 receives key dormancy instruction input by user when status information is lock state information.
For security consideration, the function that the key of a key suspend mode unmanned plane/mono- wakes up unmanned plane is increased at intelligent terminal.
When above-mentioned status information is lock state information, intelligent terminal can receive key dormancy instruction input by user.In intelligence
The physical button for controlling one key suspend mode of unmanned plane or key wake-up, or the nothing in intelligent terminal can be provided in terminal
The virtual key of control one key suspend mode of unmanned plane or key wake-up is provided in Human-machine Control APP.User can pass through the physics
Button or virtual key input suspend mode wake up instruction.
In view of unmanned plane there are various not expected emergency cases in flight course or during ground alert,
In order to ensure that user can cope with emergency case, brief reaction time, in the process of flight by manually controlling at the first time
In a key suspend mode aircraft cannot be set, therefore only can just be received input by user when status information is lock state information
One key dormancy instruction.Be provided in the unmanned aerial vehicle (UAV) control APP of intelligent terminal control one key suspend mode of unmanned plane or a key wake up
The virtual key, which automatically becomes, for virtual key, after aircrafts electric machinery unlock and in state of flight can not change state, no
It can be switched to dormant state.
Step S206 sends suspend mode to the connection equipment between the control system or control system and intelligent terminal of unmanned plane
Order, so that control system or connection equipment enter dormant state.
Intelligent terminal after obtaining above-mentioned key dormancy instruction, need to the control system of unmanned plane or the control system with
Connection equipment between intelligent terminal sends sleep command.The control system of unmanned plane include unmanned plane flight control system or
Electron speed regulator, connection equipment includes base station or day dead end.After above-mentioned control system or connection equipment enter dormant state, nothing
It is man-machine to unlock.
Step S208 is called out when receiving key wake-up instruction input by user to control system or connection equipment transmission
It wakes up and orders, so that control system or connection equipment exit dormant state.
After controlling unmanned plane suspend mode, user can also input a key by intelligent terminal and wake up instruction, and intelligence is whole at this time
It holds to control system or connection equipment and sends wake-up command, so that control system or connection equipment exit dormant state.It is moving back
After going out dormant state, unmanned plane can be unlocked and be taken off with normal release, motor.
The control method of above-mentioned unmanned plane provided in an embodiment of the present invention, increased at intelligent terminal a key suspend mode nobody
The key of machine/mono- wakes up the function of unmanned plane, and when unmanned plane is in the lock state, intelligent terminal can receive a key input by user
Dormancy instruction, and send above-mentioned suspend mode life to the connection equipment between the control system or control system and intelligent terminal of unmanned plane
It enables, so that control system or connection equipment enter dormant state, under the dormant state, unmanned plane can not unlock, to subtract
It is unexpected caused by few dangerous unlock, additional safety guarantee is provided.
In the dormant state, it cannot unlock and take off, but holder and camera function can be used normally, i.e., dormancy instruction is not
Limit holder and camera.The manipulation of holder and camera will not bring emergency case or personal injury, so need not be in suspend mode control
The range of system, it is possible to reduce the difficulty of design.In the hibernation mode, holder is controllable, camera video recording capable of taking pictures.Above-mentioned work(can be used
The scene of energy may include following situations：Unmanned plane landing locks, when checking Air Diary or camera shooting file；Unmanned plane
Under stationary state, is taken pictures using camera and (be equally applicable to holder and camera under development phase static condition to test) when recording a video.
The flow chart of the control method of unmanned plane shown in Figure 3 enters dormant state with the control system of unmanned plane
For illustrate, include the following steps：
Step S302, intelligent terminal connects unmanned plane, and receives the status information of unmanned plane.
Step S304 judges whether the status information is lock state information.If so, executing step S306；If not,
Execute step S308.
In order to confirm whether the current state of unmanned plane can need to judge the state of unmanned plane into suspend mode,
Only at which when lock-out state, dormancy instruction input by user can be just received.Intelligent terminal is provided with a key suspend mode and presses
Button and a key wake up button, can be virtual key or physical button, and the key suspend mode button and a key wake up button can be with
Can also be two independent buttons or button using the same button or button.
Step S306 receives key dormancy instruction input by user.In the case where the judging result of above-mentioned steps is to be,
Intelligent terminal can receive key dormancy instruction input by user.
One key suspend mode button is set as invalid by step S308.Such as set virtual key to change state, this
When user can not input dormancy instruction.
Step S310 sends sleep command, so that the control system enters dormant state to the control system of unmanned plane.
The flight control system of unmanned plane can receive the sleep command that intelligent terminal is sent by sky end, which refers to
Order can be by the forwarding of base station.After receiving the sleep command, flight control system can refuse to receive any unlock and refer to
It enables and flight rod volume instructs, until receiving the wake-up command of intelligent terminal transmission；After receiving the sleep command, fly
Row control system can also send lock instruction to electron speed regulator, after electron speed regulator normally receives the locked instruction,
No longer receive any motor unlock instruction and the instruction of flight rod volume, until receiving wake-up command.Enter in control system
After dormant state, when user's operation remote controler carries out toed-in unlock unmanned plane, motor does not rotate, and can not unlock.General unlock
Operation is carried out by controlling throttle lever or steering yoke, and refusal rod volume instruction can also make unmanned plane that can not unlock.
After control system enters dormant state, when being input operation instruction at remote controler, remote controler can send out vibrations
The flicker extremely of the machine wall lamp of alarm or unmanned plane is alarmed to illustrate to be now in dormant state.
Step S312 receives a key input by user and wakes up instruction.After the control system of unmanned plane enters dormant state,
User can also wake up the unmanned plane by one key of intelligent terminal.
Step S314 sends wake-up command, so that control system exits dormant state to the control system.
After control system receives the wake-up command, flight control system can release stopping for itself or electron speed regulator
Dormancy state receives motor unlock instruction and the instruction of flight rod volume, and unmanned plane can be taken off with normal release at this time.For example, can grasp
Make remote controler and carry out toed-in unlock aircraft, motor normally starts, unlocks successfully.
The control method of above-mentioned unmanned plane provided in an embodiment of the present invention, increased at intelligent terminal a key suspend mode nobody
The key of machine/mono- wakes up the function of unmanned plane, and when intelligent terminal sends sleep command to the control system of unmanned plane, unmanned plane flies
Row control system or electron speed regulator enter dormant state, no longer receive any motor unlock instruction and the instruction of flight rod volume, directly
Until receiving wake-up command, it is possible to reduce it is unexpected caused by dangerous unlock, additional safety guarantee is provided.
The flow chart of the control method of unmanned plane shown in Figure 4, method shown in Fig. 4 is with the control system of unmanned plane
Connection equipment between intelligent terminal illustrates for entering dormant state, includes the following steps：
Step S402, intelligent terminal connects unmanned plane, and receives the status information of unmanned plane.
Step S404 judges whether the status information is lock state information.If so, executing step S406；If not,
Execute step S408.
Step S406 receives key dormancy instruction input by user.
One key suspend mode button is set as invalid by step S408.
Step S410 sends sleep command, so that the control system enters dormant state to above-mentioned connection equipment.
The day dead end of base station or unmanned plane can receive the sleep command that energy terminal is sent.When receiving the sleep command
Afterwards, base station or day dead end can be transmitted with the instruction of shield electric machine unlock instruction and remote controler rod volume, make above-metioned instruction data without
Method uploads to the flight control system of unmanned plane, until receiving wake-up command.After connection equipment enters dormant state,
When user's operation remote controler carries out toed-in unlock unmanned plane, motor does not rotate, and can not unlock.
Step S412 receives a key input by user and wakes up instruction.After connection equipment enters dormant state, user may be used also
To wake up the unmanned plane by one key of intelligent terminal.
Step S414 sends wake-up command to the control system, so that connection equipment exits dormant state.
After control system receives the wake-up command, flight control system can release stopping for itself or electron speed regulator
Dormancy state receives motor unlock instruction and the instruction of flight rod volume, and unmanned plane can be taken off with normal release at this time.For example, can grasp
Make remote controler and carry out toed-in unlock aircraft, motor normally starts, unlocks successfully.
The control method of above-mentioned unmanned plane provided in an embodiment of the present invention, increased at intelligent terminal a key suspend mode nobody
The key of machine/mono- wakes up the function of unmanned plane, the connection equipment between control system and intelligent terminal of the intelligent terminal to unmanned plane
Send sleep command when, the day dead end of base station or unmanned plane enters dormant state, no longer receive any motor unlock instruction and
Flight rod volume instructs, until receiving wake-up command, it is possible to reduce and it is unexpected caused by dangerous unlock, additional peace is provided
All risk insurance hinders.
Embodiment 2
An embodiment of the present invention provides a kind of control method of unmanned plane, the control methods of unmanned plane shown in Figure 5
Flow chart, this method comprises the following steps：
Step S502, unmanned plane boot up self-test.
After unmanned plane booting, default conditions are dormant state.When control system or connection equipment in a dormant state when,
Dormant state prompt is added in the self-detection result of output.The self-test of this function can be added at the self-test interface of intelligent terminal
As a result, voice prompt user unmanned plane is now arranged in dormant state after the completion of self-test, wake operation please be execute before unlock.
Step S504, intelligent terminal receives suspend mode account information input by user, and is stepped on by suspend mode account information
Record.
Step S506, unmanned plane connect with intelligent terminal and with the suspend mode account information mutual authentication.
After intelligent terminal logins successfully, the control system connection of intelligent terminal and unmanned plane is authenticated.Intelligent terminal is logical
The login of certain account is crossed, and one key wake-up can only be carried out again by the account provided with after a key suspend mode to the unmanned plane of connection
Operation.In order to ensure validity, the function cannot be controlled in the same direction between different accounts.
Therefore if do not waken up first after suspend mode, unmanned plane will be unable to unlock flight, other people cannot use, so as to
To avoid the loss of aircraft by a key suspend mode unmanned plane.
Step S508 receives key dormancy instruction input by user.
Step S510 sends suspend mode to the connection equipment between the control system or control system and intelligent terminal of unmanned plane
Order, so that control system or connection equipment enter dormant state.
Step S512 is called out when receiving key wake-up instruction input by user to control system or connection equipment transmission
It wakes up and orders, so that control system or connection equipment exit dormant state.
The control method of above-mentioned unmanned plane provided in an embodiment of the present invention, increased at intelligent terminal a key suspend mode nobody
The key of machine/mono- wakes up the function of unmanned plane, and first passing through account in advance in intelligent terminal logs in and complete certification with unmanned plane, after suspend mode
It is only capable of carrying out a key wake operation again by the account, improves the theft protection ability of unmanned plane.
Embodiment 3
An embodiment of the present invention provides a kind of control devices of unmanned plane, are applied to the intelligent terminal of control unmanned plane, ginseng
The structure diagram of the control device of unmanned plane as shown in Figure 6, including：
State information acquisition module 61, for when the control system of intelligent terminal and unmanned plane is in connection status, obtaining
Take the status information of unmanned plane；
Command reception module 62, for when status information is lock state information, receiving key suspend mode input by user
Instruction；
Sleep block 63, for being sent out to the connection equipment between the control system or control system and intelligent terminal of unmanned plane
Sleep command is sent, so that control system or connection equipment enter dormant state；In the dormant state, unmanned plane can not unlock；
Wake-up module 64, for when receiving key wake-up instruction input by user, to control system or connecting equipment
Wake-up command is sent, so that control system or connection equipment exit dormant state.
Wherein, control system includes the flight control system or electron speed regulator of unmanned plane；Connection equipment include base station or
Its dead end.
The structure diagram of the control device of unmanned plane shown in Figure 7, above-mentioned apparatus further include authentication module 71, are used for
Receive suspend mode account information input by user；It is logged according to suspend mode account information, and connects intelligent terminal and unmanned plane
Control system is authenticated.
The structure diagram of the control device of unmanned plane shown in Figure 8, above-mentioned apparatus further include login module 81, are used for
It is logged in by the account for suspend mode.
Above-mentioned intelligent terminal is provided with a key suspend mode button, the structural frames of the control device of unmanned plane shown in Figure 9
Figure, above-mentioned apparatus further include：Invalid setup module 91 is used for when status information is non-locking state information, by a key suspend mode
Button is set as invalid.
The structure diagram of the control device of unmanned plane shown in Figure 10, above-mentioned apparatus further include：Selftest module 11 is used
In when control system or connection equipment in a dormant state when, in the self-detection result of output add dormant state prompt.
The control device of above-mentioned unmanned plane provided in an embodiment of the present invention, increased at intelligent terminal a key suspend mode nobody
The key of machine/mono- wakes up the function of unmanned plane, and when unmanned plane is in the lock state, intelligent terminal can receive a key input by user
Dormancy instruction, and send above-mentioned suspend mode life to the connection equipment between the control system or control system and intelligent terminal of unmanned plane
It enables, so that control system or connection equipment enter dormant state, under the dormant state, unmanned plane can not unlock, to subtract
It is unexpected caused by few dangerous unlock, additional safety guarantee is provided.
The embodiment of the present invention additionally provides a kind of intelligent terminal, including processor, memory, bus and communication interface, should
Processor, communication interface and memory are connected by bus；The memory is for storing program；The processor is for passing through bus
Program stored in memory is called, the method that above-described embodiment provides is executed.
The embodiment of the present invention additionally provides a kind of computer of non-volatile program code that can perform with processor can
Medium is read, program code makes the method that processor executes above-described embodiment offer.
It should be noted that each embodiment in this specification is described in a progressive manner, each embodiment weight
Point explanation is all difference from other examples, and the same or similar parts between the embodiments can be referred to each other.
The technique effect of the control device and intelligent terminal for the unmanned plane that the embodiment of the present invention is provided, realization principle and generation is with before
It is identical to state embodiment of the method, to briefly describe, device embodiment part does not refer to place, can refer to phase in preceding method embodiment
Answer content.
In several embodiments provided herein, it should be understood that disclosed device and method can also pass through
Other modes are realized.The apparatus embodiments described above are merely exemplary, for example, the flow chart in attached drawing and block diagram
Show the device of multiple embodiments according to the present invention, the architectural framework in the cards of method and computer program product,
Function and operation.In this regard, each box in flowchart or block diagram can represent the one of a module, section or code
Part, a part for the module, section or code, which includes that one or more is for implementing the specified logical function, to be held
Row instruction.It should also be noted that at some as in the realization method replaced, the function of being marked in box can also be to be different from
The sequence marked in attached drawing occurs.For example, two continuous boxes can essentially be basically executed in parallel, they are sometimes
It can execute in the opposite order, this is depended on the functions involved.It is also noted that every in block diagram and or flow chart
The combination of box in a box and block diagram and or flow chart can use function or the dedicated base of action as defined in executing
It realizes, or can be realized using a combination of dedicated hardware and computer instructions in the system of hardware.
It, can be with if above-mentioned function is realized in the form of SFU software functional unit and when sold or used as an independent product
It is stored in a computer read/write memory medium.Based on this understanding, technical scheme of the present invention is substantially in other words
The part of the part that contributes to existing technology or the technical solution can be expressed in the form of software products, the meter
Calculation machine software product is stored in a storage medium, including some instructions are used so that a computer equipment (can be
People's computer, server or network equipment etc.) it performs all or part of the steps of the method described in the various embodiments of the present invention.
And storage medium above-mentioned includes：USB flash disk, mobile hard disk, read-only memory (ROM, Read-Only Memory), arbitrary access are deposited
The various media that can store program code such as reservoir (RAM, Random Access Memory), magnetic disc or CD.
Finally it should be noted that：Embodiment described above, only specific implementation mode of the invention, to illustrate the present invention
Technical solution, rather than its limitations, scope of protection of the present invention is not limited thereto, although with reference to the foregoing embodiments to this hair
It is bright to be described in detail, it will be understood by those of ordinary skill in the art that：Any one skilled in the art
In the technical scope disclosed by the present invention, it can still modify to the technical solution recorded in previous embodiment or can be light
It is readily conceivable that variation or equivalent replacement of some of the technical features；And these modifications, variation or replacement, do not make
The essence of corresponding technical solution is detached from the spirit and scope of technical solution of the embodiment of the present invention, should all cover the protection in the present invention
Within the scope of.Therefore, protection scope of the present invention should be based on the protection scope of the described claims.
Claims (10)
1. a kind of control method of unmanned plane, which is characterized in that it is applied to the intelligent terminal of control unmanned plane, including：
When the control system of the intelligent terminal and the unmanned plane is in connection status, the state letter of the unmanned plane is obtained
Breath；
When the status information is lock state information, key dormancy instruction input by user is received；
Suspend mode is sent to the connection equipment between the control system or the control system and the intelligent terminal of the unmanned plane
Order, so that the control system or the connection equipment enter dormant state；In the hibernate state, the unmanned plane
It can not unlock；
When receiving the key wake-up instruction input by user, sends and wake up to the control system or the connection equipment
Order, so that the control system or the connection equipment exit dormant state.
2. according to the method described in claim 1, it is characterized in that, the control system includes the flight control of the unmanned plane
System or electron speed regulator；The connection equipment includes base station or day dead end.
3. according to the method described in claim 1, it is characterized in that, the status information for obtaining the unmanned plane the step of
Before, further include：
Receive suspend mode account information input by user；
It is logged according to the suspend mode account information, and the control system for connecting the intelligent terminal and the unmanned plane carries out
Certification.
4. according to the method described in claim 1, it is characterized in that, being called out to the control system or connection equipment transmission
It wakes up and orders, so that before the step of control system or the connection equipment exit dormant state, further include：
It is logged in by the account for suspend mode.
5. according to the method described in claim 1, it is characterized in that, the intelligent terminal is provided with a key suspend mode button；It is described
Method further includes：
When the status information is non-locking state information, the key suspend mode button is set as invalid.
6. according to the method described in claim 1, it is characterized in that, the method further includes：
When the control system or the connection equipment in a dormant state when, in the self-detection result of output add suspend mode shape
State prompts.
7. a kind of control device of unmanned plane, which is characterized in that it is applied to the intelligent terminal of control unmanned plane, including：
State information acquisition module is used for when the control system of the intelligent terminal and the unmanned plane is in connection status,
Obtain the status information of the unmanned plane；
Command reception module, for when the status information is lock state information, receiving key suspend mode input by user and referring to
It enables；
Sleep block is used for the connection between the control system or the control system and the intelligent terminal of the unmanned plane
Equipment sends sleep command, so that the control system or the connection equipment enter dormant state；In the dormant state
Under, the unmanned plane can not unlock；
Wake-up module, for when receiving the key input by user and waking up instruction, to the control system or the company
It connects equipment and sends wake-up command, so that the control system or the connection equipment exit dormant state.
8. device according to claim 7, which is characterized in that the control system includes the flight control of the unmanned plane
System or electron speed regulator；The connection equipment includes base station or day dead end.
9. a kind of intelligent terminal, which is characterized in that including processor, memory, bus and communication interface, the processor leads to
Letter interface is connected with memory by the bus；
The memory is for storing program；
The processor, for calling the program being stored in the memory, perform claim that 1-6 is required to appoint by the bus
Method described in one.
10. a kind of computer-readable medium for the non-volatile program code that can perform with processor, which is characterized in that described
Program code makes the processor perform claim require 1-6 any one of them methods.
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| CN201810239165.2A CN108490964A (en) | 2018-03-21 | 2018-03-21 | Control method, device and the intelligent terminal of unmanned plane |
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| CN201810239165.2A CN108490964A (en) | 2018-03-21 | 2018-03-21 | Control method, device and the intelligent terminal of unmanned plane |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110032414A (en) * | 2019-03-06 | 2019-07-19 | 联想企业解决方案(新加坡)有限公司 | Apparatus and method for secure user authentication in remote console mode |
| CN112154407A (en) * | 2019-08-13 | 2020-12-29 | 深圳市大疆创新科技有限公司 | Terminal control method, control terminal and movable platform |
| WO2021003691A1 (en) * | 2019-07-10 | 2021-01-14 | 深圳市大疆创新科技有限公司 | Gimbal and camera control method and apparatus |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS62204315A (en) * | 1986-03-05 | 1987-09-09 | Fanuc Ltd | Control system for unmanned carrier |
| CN105320903A (en) * | 2015-09-30 | 2016-02-10 | 杨毅 | Electronic device and data reading and writing method based on the electronic device |
| CN105539869A (en) * | 2016-02-03 | 2016-05-04 | 辽宁猎鹰航空科技有限公司 | Unmanned aerial vehicle maintenance and management system and method |
| CN106375396A (en) * | 2016-08-30 | 2017-02-01 | 乐视控股（北京）有限公司 | Method and device for dormancy and awakening of vehicle-mounted intelligent terminal |
| CN206894795U (en) * | 2017-05-23 | 2018-01-16 | 深圳市道通智能航空技术有限公司 | A kind of remote control for realizing image procossing and unmanned flight's system |
-
2018
- 2018-03-21 CN CN201810239165.2A patent/CN108490964A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS62204315A (en) * | 1986-03-05 | 1987-09-09 | Fanuc Ltd | Control system for unmanned carrier |
| CN105320903A (en) * | 2015-09-30 | 2016-02-10 | 杨毅 | Electronic device and data reading and writing method based on the electronic device |
| CN105539869A (en) * | 2016-02-03 | 2016-05-04 | 辽宁猎鹰航空科技有限公司 | Unmanned aerial vehicle maintenance and management system and method |
| CN106375396A (en) * | 2016-08-30 | 2017-02-01 | 乐视控股（北京）有限公司 | Method and device for dormancy and awakening of vehicle-mounted intelligent terminal |
| CN206894795U (en) * | 2017-05-23 | 2018-01-16 | 深圳市道通智能航空技术有限公司 | A kind of remote control for realizing image procossing and unmanned flight's system |
Non-Patent Citations (1)
| Title |
|---|
| 徐德，等: "PLC在机械手控制中的应用", 《可编程序控制器（PLC）应用技术》 * |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110032414A (en) * | 2019-03-06 | 2019-07-19 | 联想企业解决方案(新加坡)有限公司 | Apparatus and method for secure user authentication in remote console mode |
| CN110032414B (en) * | 2019-03-06 | 2023-06-06 | 联想企业解决方案(新加坡)有限公司 | Apparatus and method for secure user authentication in remote console mode |
| WO2021003691A1 (en) * | 2019-07-10 | 2021-01-14 | 深圳市大疆创新科技有限公司 | Gimbal and camera control method and apparatus |
| US11323622B2 (en) | 2019-07-10 | 2022-05-03 | SZ DJI Technology Co., Ltd. | Gimbal, method and apparatus for controlling photographing apparatus |
| CN112154407A (en) * | 2019-08-13 | 2020-12-29 | 深圳市大疆创新科技有限公司 | Terminal control method, control terminal and movable platform |
| WO2021026776A1 (en) * | 2019-08-13 | 2021-02-18 | 深圳市大疆创新科技有限公司 | Terminal control method, control terminal and movable platform |
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