CN108357693A - A kind of low cost is tethered at light-duty multi-rotor unmanned aerial vehicle system and its working method - Google Patents
A kind of low cost is tethered at light-duty multi-rotor unmanned aerial vehicle system and its working method Download PDFInfo
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- CN108357693A CN108357693A CN201810393221.8A CN201810393221A CN108357693A CN 108357693 A CN108357693 A CN 108357693A CN 201810393221 A CN201810393221 A CN 201810393221A CN 108357693 A CN108357693 A CN 108357693A
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- Prior art keywords
- power supply
- tethered
- unmanned aerial
- aerial vehicle
- supply system
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- Pending
Links
- 238000000034 method Methods 0.000 title claims abstract description 9
- 230000005611 electricity Effects 0.000 claims description 13
- 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 10
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 7
- 229910052782 aluminium Inorganic materials 0.000 claims description 7
- 239000004411 aluminium Substances 0.000 claims description 7
- 238000012546 transfer Methods 0.000 claims description 6
- 238000005183 dynamical system Methods 0.000 claims description 5
- 238000010146 3D printing Methods 0.000 claims description 4
- 229910052799 carbon Inorganic materials 0.000 claims description 4
- 239000002131 composite material Substances 0.000 claims description 4
- 239000002657 fibrous material Substances 0.000 claims description 4
- 229910002804 graphite Inorganic materials 0.000 claims description 4
- 239000010439 graphite Substances 0.000 claims description 4
- 238000010248 power generation Methods 0.000 claims description 2
- 238000004891 communication Methods 0.000 abstract description 8
- 238000012544 monitoring process Methods 0.000 abstract description 5
- 230000007774 longterm Effects 0.000 abstract description 3
- 238000013507 mapping Methods 0.000 abstract description 3
- 238000011160 research Methods 0.000 abstract description 3
- 238000012806 monitoring device Methods 0.000 abstract description 2
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 2
- 229910052744 lithium Inorganic materials 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000011840 criminal investigation Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000003786 synthesis reaction Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F3/00—Ground installations specially adapted for captive aircraft
- B64F3/02—Ground installations specially adapted for captive aircraft with means for supplying electricity to aircraft during flight
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- 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
- H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
- H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Power Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The present invention provides a kind of low cost and is tethered at light-duty multi-rotor unmanned aerial vehicle system and its working method, the system it include drone body, cable, earth station and power supply system；The power supply system is connect by cable with drone body；The drone body is connect with earth station system.Possess longer cruise duration while having multi-rotor aerocraft all advantages, the several working ways such as fixed, vehicle-mounted removable and carrier-borne movable type can also be compatible with.The continual aerial monitoring of a variety of long-times and communication are can be applied to, provides platform steady in a long-term for a variety of Image-forming instruments, monitoring device and emergency communication trunking, the in particular departments such as the limited scientific research of funds, mapping provide new way.
Description
Technical field
The invention belongs to UAV system, and in particular to a kind of low cost is tethered at light-duty multi-rotor unmanned aerial vehicle system and its work
Make method.
Background technology
Multi-rotor unmanned aerial vehicle flight stability manipulates simply, and it is flat that reliable space base can be provided for fixed point monitoring electronics
Platform widely applies to the fields such as military affairs, criminal investigation, media, amusement, communication, environment monitoring.Existing light-duty more rotors without
Man-machine power supply almost all uses self-contained lithium battery.The finite energy of lithium battery need to supply unmanned plane dynamical system,
Clouds terrace system and wireless data sending dispatch control system, constrain Aircraft Conceptual Design to a certain extent.In general, most light-duty more rotations
Wing unmanned plane is within 40 minutes cruise duration, and has strict demand to carrying load.Meanwhile unmanned plane during flying power is by energy
Source influences greatly, to be difficult to control in relatively strong winds load environment.In addition, unmanned plane energy resource supply also influences its interference free performance
And communication capacity, control link, which is interfered, results in most civilian light-duty unmanned plane during flying accidents.It is by nothing to be tethered at unmanned plane
Man-machine and tether cable combines the UAV system of realization, and electric energy is transmitted by Aviation cable, so solve it is conventional nobody
Function source restriction problem, provides longer-term stabilised platform, and this mode can meet certain special operation condition requirements.
Invention content
The object of the present invention is to provide a kind of low costs to be tethered at light-duty multi-rotor unmanned aerial vehicle system and its working method.
The present invention uses following technical scheme：A kind of low cost is tethered at light-duty multi-rotor unmanned aerial vehicle system comprising nobody
Machine ontology, cable, earth station and power supply system；The power supply system is connect by cable with drone body；Institute
Drone body is stated to connect with earth station system.
In an embodiment of the present invention, the drone body includes that shell and the electricity being arranged on shell are adjusted, fly control system
System, Data transfer system, GPS positioning system, rectifier；The rectifier passes through cable connection with power supply system.
The blade and supporting structure of the shell are molded by composite graphite olefinic carbon fibrous material 3D printing.
In an embodiment of the present invention, the flight control system selects APM2.8 model flight control systems；The Data transfer system choosing
With 433MZH model data radio stations；The electricity is tuned with Hobbywing 30A electricity tune；The GPS positioning system selects Ublox-
7M GPS positioning modules.
In an embodiment of the present invention, the power supply system is fixed power supply system, vehicle-mounted removable electricity
Source supply system or carrier-borne mobile power supply system.
In an embodiment of the present invention, the power supply system is vehicle-mounted removable power supply system；It is described vehicle-mounted
Mobile power supply system includes Vehicular solar generator, accumulator and vehicle-mounted inverter；The Vehicular solar power generation
Machine is exported to be connected with accumulator input；The accumulator output is connected with vehicle-mounted inverter input；The vehicle-mounted inverter output
It is connect with drone body.
The present invention also provides a kind of low costs to be tethered at light-duty multi-rotor unmanned aerial vehicle system working method, passes through earth station pair
UAV system carries out trajectory planning and state modulator；Inversion is passed sequentially through by the solar generator of power supply system
Device, aluminium cable, rectifier are powered to UAV system；The power supply system dynamical system then Mobile portable formula
220 V alternating currents supply, and are transmitted by conventional aluminium cable, and it is unmanned electromechanical to convert 12 V DC powereds through airborne lightweight rectifier
Machine；UAV system selects APM2.8 models flight control system and 433MZH model data radio stations, using Hobbywing 30A electricity
It adjusts, Ublox-7M GPS positioning modules, unmanned aerial vehicle stand control module is selected to select Mission Planner.
Compared with prior art, the present invention provides a set of low cost and is tethered at UAV system, is having multi-rotor aerocraft
Possess longer cruise duration while all advantages, it is more that fixed, vehicle-mounted removable and carrier-borne movable type etc. can also be compatible with
Kind working method.The continual aerial monitoring of a variety of long-times and communication are can be applied to, is a variety of Image-forming instruments, monitoring device
Platform steady in a long-term is provided with emergency communication trunking, the in particular departments such as the limited scientific research of funds, mapping provide new way
Diameter.
Description of the drawings
Fig. 1 is the primary structure schematic diagram of the present invention.
Specific implementation mode
Explanation is further explained to the present invention in the following with reference to the drawings and specific embodiments.
A kind of low cost is tethered at light-duty multi-rotor unmanned aerial vehicle system comprising drone body, cable, earth station and power supply
Feed system；The power supply system is connect by cable with drone body；The drone body and earth station system
Connection.
In an embodiment of the present invention, the drone body includes that shell and the electricity being arranged on shell are adjusted, fly control system
System, Data transfer system, GPS positioning system, rectifier；The rectifier passes through cable connection with power supply system；For will be electric
The alternating current of source supply system is converted to direct current.
The blade and supporting structure of the shell are molded by composite graphite olefinic carbon fibrous material 3D printing.
In an embodiment of the present invention, the flight control system selects APM2.8 model flight control systems；The Data transfer system choosing
With 433MZH model data radio stations；The electricity is tuned with Hobbywing 30A electricity tune；The GPS positioning system selects Ublox-
7M GPS positioning modules.
The present invention also provides a kind of low costs to be tethered at light-duty multi-rotor unmanned aerial vehicle system working method, passes through earth station pair
UAV system carries out trajectory planning and state modulator；Inversion is passed sequentially through by the solar generator of power supply system
Device, aluminium cable, rectifier are powered to UAV system；The power supply system dynamical system then Mobile portable formula
220 V alternating currents supply, and are transmitted by conventional aluminium cable, and it is unmanned electromechanical to convert 12 V DC powereds through airborne lightweight rectifier
Machine；UAV system selects APM2.8 models flight control system and 433MZH model data radio stations, using Hobbywing 30A electricity
It adjusts, Ublox-7M GPS positioning modules, unmanned aerial vehicle stand control module is selected to select Mission Planner.
In a specific embodiment of the invention, dynamical system then uses 220 V alternating currents of Mobile portable formula to supply, by routine
Aluminium cable transmits, and 12 V dc powered drive motors are converted through airborne lightweight rectifier.Unmanned plane overall dimensions 400 × 400 ×
260 mm, 500 mm of wheelbase, blade and supporting structure are molded by composite graphite olefinic carbon fibrous material 3D printing, to ensure unmanned plane
With preferable heat dissipation performance.APM2.8 models flight control system and 433MZH model data radio stations are selected, using Hobbywing
30A electricity tune selects Ublox-7M GPS positioning modules, Unmanned Aircraft Control Stations Control System to select Mission Planner.At this
In invention specific embodiment, unmanned plane during flying part total quality 800 g, 20 m of reliable flying height, reliable flying radius 10
M, 2.0 hours max-endurances, system synthesis is relatively low.The low cost of the present invention is tethered at UAV system, is having more rotors
Possess longer cruise duration while aircraft all advantages, fixed, vehicle-mounted removable and carrier-borne movement can also be compatible with
The several working ways such as formula.The continual aerial monitoring of a variety of long-times and communication are can be applied to, is a variety of Image-forming instruments, prison
Measurement equipment and emergency communication trunking provide platform steady in a long-term, and the in particular departments such as the limited scientific research of funds, mapping provide
New way.
The above are preferred embodiments of the present invention, all any changes made according to the technical solution of the present invention, and generated function is made
When with range without departing from technical solution of the present invention, all belong to the scope of protection of the present invention.
Claims (7)
1. a kind of low cost is tethered at light-duty multi-rotor unmanned aerial vehicle system, it is characterised in that：Including drone body, cable, ground
It stands and power supply system；The power supply system is connect by cable with drone body；The drone body and ground
Face station passes through wireless network connection.
2. low cost according to claim 1 is tethered at light-duty multi-rotor unmanned aerial vehicle system, it is characterised in that：The unmanned plane
Ontology includes shell and the electric tune, flight control system, Data transfer system, GPS positioning system, the rectifier that are arranged on shell；It is described whole
Stream device passes through cable connection with power supply system.
3. low cost according to claim 2 is tethered at light-duty multi-rotor unmanned aerial vehicle system, it is characterised in that：The shell
Blade and supporting structure by composite graphite olefinic carbon fibrous material 3D printing be molded.
4. low cost according to claim 2 is tethered at light-duty multi-rotor unmanned aerial vehicle system, it is characterised in that：The winged control system
System selects APM2.8 model flight control systems；The Data transfer system selects 433MZH model data radio stations；The electricity tunes use
Hobbywing 30A electricity tune；The GPS positioning system selects Ublox-7M GPS positioning modules.
5. low cost according to claim 1 is tethered at light-duty multi-rotor unmanned aerial vehicle system, it is characterised in that：The power supply supplies
It is fixed power supply system, vehicle-mounted removable power supply system or carrier-borne mobile power supply system to system.
6. low cost according to claim 1 is tethered at light-duty multi-rotor unmanned aerial vehicle system, it is characterised in that：The power supply supplies
It is vehicle-mounted removable power supply system to system；The vehicle-mounted removable power supply system includes Vehicular solar power generation
Machine, accumulator and vehicle-mounted inverter；The Vehicular solar generator output is connected with accumulator input；The accumulator output
It inputs and connects with vehicle-mounted inverter；The vehicle-mounted inverter output is connect with drone body.
7. one kind being tethered at light-duty multi-rotor unmanned aerial vehicle system working method based on low cost described in claim 1, feature exists
In：Trajectory planning and state modulator are carried out to UAV system by earth station；It is sent out by the solar energy of power supply system
Motor passes sequentially through inverter, aluminium cable, rectifier and is powered to UAV system；The power supply system dynamical system
Then 220 V alternating currents of Mobile portable formula supply system, are transmitted by conventional aluminium cable, and 12 V direct currents are converted through airborne lightweight rectifier
Electric drive unmanned plane motor；UAV system selects APM2.8 models flight control system and 433MZH model data radio stations, uses
Hobbywing 30A electricity tune selects Ublox-7M GPS positioning modules, unmanned aerial vehicle stand control module to select Mission
Planner。
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810393221.8A CN108357693A (en) | 2018-04-27 | 2018-04-27 | A kind of low cost is tethered at light-duty multi-rotor unmanned aerial vehicle system and its working method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810393221.8A CN108357693A (en) | 2018-04-27 | 2018-04-27 | A kind of low cost is tethered at light-duty multi-rotor unmanned aerial vehicle system and its working method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108357693A true CN108357693A (en) | 2018-08-03 |
Family
ID=63009273
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810393221.8A Pending CN108357693A (en) | 2018-04-27 | 2018-04-27 | A kind of low cost is tethered at light-duty multi-rotor unmanned aerial vehicle system and its working method |
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| Country | Link |
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| CN (1) | CN108357693A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201576944U (en) * | 2009-12-07 | 2010-09-08 | 浙江光益光能科技有限公司 | Vehicular solar energy mobile power supply |
| CN103144779A (en) * | 2012-11-30 | 2013-06-12 | 中国电子科技集团公司第七研究所 | Multi-rotor-wing unmanned aerial vehicle mooring system |
| CN104859854A (en) * | 2015-04-16 | 2015-08-26 | 北京航空航天大学 | Heavy-load low-structure-complexity double-coaxial-twin-rotor unmanned aerial vehicle |
| CN107108024A (en) * | 2014-11-10 | 2017-08-29 | 上升航空***股份有限公司 | Nolo flight device |
| CN107512391A (en) * | 2017-08-23 | 2017-12-26 | 长春长光精密仪器集团有限公司 | Based on the rotor unmanned aircraft for being tethered at cable power supply |
| CN107826266A (en) * | 2017-11-08 | 2018-03-23 | 珠海市双捷科技有限公司 | It is tethered at ground handling station and is tethered at UAS |
-
2018
- 2018-04-27 CN CN201810393221.8A patent/CN108357693A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201576944U (en) * | 2009-12-07 | 2010-09-08 | 浙江光益光能科技有限公司 | Vehicular solar energy mobile power supply |
| CN103144779A (en) * | 2012-11-30 | 2013-06-12 | 中国电子科技集团公司第七研究所 | Multi-rotor-wing unmanned aerial vehicle mooring system |
| CN107108024A (en) * | 2014-11-10 | 2017-08-29 | 上升航空***股份有限公司 | Nolo flight device |
| CN104859854A (en) * | 2015-04-16 | 2015-08-26 | 北京航空航天大学 | Heavy-load low-structure-complexity double-coaxial-twin-rotor unmanned aerial vehicle |
| CN107512391A (en) * | 2017-08-23 | 2017-12-26 | 长春长光精密仪器集团有限公司 | Based on the rotor unmanned aircraft for being tethered at cable power supply |
| CN107826266A (en) * | 2017-11-08 | 2018-03-23 | 珠海市双捷科技有限公司 | It is tethered at ground handling station and is tethered at UAS |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180803 |
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| RJ01 | Rejection of invention patent application after publication |