CN104828252A - Method for implementing aerial continuous voyage for unmanned aerial vehicle - Google Patents

Method for implementing aerial continuous voyage for unmanned aerial vehicle Download PDF

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Publication number
CN104828252A
CN104828252A CN201510293145.XA CN201510293145A CN104828252A CN 104828252 A CN104828252 A CN 104828252A CN 201510293145 A CN201510293145 A CN 201510293145A CN 104828252 A CN104828252 A CN 104828252A
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China
Prior art keywords
charging
aircraft
wireless
unmanned aerial
aerial vehicle
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Pending
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CN201510293145.XA
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Chinese (zh)
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冯圣冰
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冯圣冰
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Priority to CN201510293145.XA priority Critical patent/CN104828252A/en
Publication of CN104828252A publication Critical patent/CN104828252A/en
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    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Abstract

The invention discloses a method for implementing aerial continuous voyage for an unmanned aerial vehicle. The method comprises a charging receiving aircraft, a wireless receiving module, a receiving control module, a battery pack, an energy supply outputting module, a charging implementing aircraft, an energy battery pack, an emission control module, a wireless emitting module and a wireless charging effective area. In the charging process, the charging receiving aircraft only needs to be kept in the wireless charging effective area produced by the charging implementing aircraft. The unmanned aerial vehicle can implement charging in the wireless coverage range without physical connection limitation and does not need to return to an airport to land, a plurality of unmanned aerial vehicles can be charged at the same time within the power allowed range, the interference of weather is small, the flying operation difficulty can be effectively lowered, and the method has the revolutionary significance in improving the cruising ability of the unmanned aerial vehicle.

Description

A kind of method that electronic unmanned aerial vehicle is continued a journey in the air
Technical field
The present invention relates to unmanned aerial vehicle design field namely to the aircraft for the purpose of special purpose, promote its duration performance, comprise increase boat time, voyage method, particularly a kind of method utilizing wireless charging skill upgrading unmanned plane duration performance.
Background technology
Along with development that is industrial and information techenology, unmanned air vehicle technique is also more and more grown up.The application of unmanned plane also gets more and more, from initial military use increasing legitimate purposes among the people till now.The power system of unmanned plane mainly contains fuel oil and electric power two kinds, current oily fuel power unmanned plane or main application at present, because it can realize very long range and the high speed of a ship or plane, and heavy load.But now along with the development of up-to-date technology, electronic unmanned plane also gets more and more in application that is military, civil area, and due to model plane motion also more and more universal, promoted the development of unmanned air vehicle technique more further.Compared with the unmanned plane of fuel power, the flying power of electronic unmanned plane is keep part in check always, on the one hand use Large Copacity, heavy-duty battery to this, but will certainly load be increased like this, higher requirement is proposed to the flight of the just little electronic unmanned plane of load own, to its speed, fuselage performance has also higher requirement, and is not directly proportional to income.Be exactly develop up-to-date technology on the other hand, improve flying power.
Summary of the invention
In order to solve the weak point in above-mentioned background technology, the object of this invention is to provide a kind of method that electronic unmanned aerial vehicle is continued a journey in the air, technical solution of the present invention is: electronic unmanned plane is in flight course, when the electric energy that self stores is not enough, send and implement charging aircraft, artificial or under automatically intervening, allow receiving charging aircraft and fly, to the wireless charging service area of implementing charging aircraft and producing, to it is characterized in that:
A) after implementing charging aircraft receiving control command, produce wireless charging service area, receive charging aircraft and receive instruction, fly to wireless charging service area, the match is successful and start charging for two-shipper;
B) in whole process of charging, two aircrafts keep relative position to stablize under automatic or artificial pattern, and can change in the spatial dimension allowed;
C) in process of charging, reception charging aircraft detects charging reception condition in real time and carries out data and returns, and ground control center regulates charging duration and charge power in real time according to return data;
D) after charging complete, receive charging aircraft and sent instruction, and depart from wireless charging service area, implement after charging aircraft receives instruction, close wireless transmission or wait for and carry out the instruction of charging to other aircrafts.
Further, all command signals and wireless signal adopt AD HOC separately, prevent interference.
Further, a frame is implemented charging aircraft can implement charging to multi-aircraft simultaneously in power allowed band.
The technological merit that the present invention has is, while uninterrupted flight, implement charging., the thorough like this labyrinth breaking away from physical connection designs and control technology, can realize multimachine and charge simultaneously, simultaneously very little by the interference that external wind, rain etc. are naturally meteorological, and when charging, the relative position between two-shipper requires very loose, this has great function to reduction flight difficulty.Wireless charging technology is applied to this field, has incomparable technological merit.
Accompanying drawing explanation
Fig. 1 is wireless charging principle of design figure of the present invention.
Detailed description of the invention
Below in conjunction with specific embodiment, the invention will be further described, is used for explaining the present invention in this illustrative examples of inventing and explanation, but not as a limitation of the invention.
When electronic unmanned plane (or model plane) is in flight course, when the electric energy that self stores is not enough, send command signal, after ground control center receives command signal, send the enforcement charging aircraft being loaded with mass energy battery.When flying to the aircraft vicinity needing to receive charging under implementing the control of charging aircraft at signal instruction, implement charging aircraft and start wireless transmission, simultaneously, under artificial or automatic the intervention, allow and receive charging aircraft and fly to implementing the wireless charging service area that produces of charging aircraft, after this sequence of operations completes, carry out wireless charging attended operation: implement charging aircraft and send matching instruction signal, receive after charging aircraft receives matching instruction signal and mate, after when two-shipper, the match is successful, wireless charging starts to carry out.In whole process of charging, two aircrafts keep relative position to stablize under automatic or artificial pattern, and can change in the spatial dimension allowed.In process of charging, reception charging aircraft detects charging reception condition in real time and carries out data and returns, and ground control center regulates charging duration in real time according to return data.When after charging complete, receive charging aircraft and send instruction, ground control center controls to accept charging aircraft and departs from wireless charging service area after receiving instruction, operating order is sent to enforcement charging aircraft simultaneously, after implementing charging aircraft reception instruction, close wireless transmission or wait for and carry out charging operations to other aircrafts.After finally completing, implement charging aircraft and give an encore, receive charging aircraft and continue to perform aerial mission.
All command signals and wireless signal adopt AD HOC separately, prevent signal disturbing.
The matching instruction signal that one frame enforcement charging aircraft sends can be received charging aircraft by multi rack and receive and mate, and can give the multi-aircraft enforcement charging that the match is successful in power allowed band simultaneously.

Claims (3)

1. the method that electronic unmanned aerial vehicle is continued a journey in the air, electronic unmanned plane is in flight course, when the electric energy that self stores is not enough, send and implement charging aircraft, under artificial or automatic the intervention, reception charging aircraft is allowed to fly, to the wireless charging service area that enforcement charging aircraft produces, to it is characterized in that:
A) after implementing charging aircraft receiving control command, produce wireless charging service area, receive charging aircraft and receive instruction, fly to wireless charging service area, the match is successful and start charging for two-shipper;
B) in whole process of charging, two aircrafts keep relative position to stablize under automatic or artificial pattern, and can change in the spatial dimension allowed;
C) in process of charging, reception charging aircraft detects charging reception condition in real time and carries out data and returns, and ground control center regulates charging duration and charge power in real time according to return data;
D) after charging complete, receive charging aircraft and sent instruction, and depart from wireless charging service area, implement after charging aircraft receives instruction, close wireless transmission or wait for and carry out the instruction of charging to other aircrafts.
2. a kind of method of continuing a journey in the air to electronic unmanned aerial vehicle according to claim 1, is characterized in that: all command signals and wireless signal adopt AD HOC separately, prevents interference.
3. a kind of method of continuing a journey in the air to electronic unmanned aerial vehicle according to claim 2, is characterized in that: charging aircraft implemented by a frame can implement charging to multi-aircraft in power allowed band simultaneously.
CN201510293145.XA 2015-06-02 2015-06-02 Method for implementing aerial continuous voyage for unmanned aerial vehicle Pending CN104828252A (en)

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Application Number Priority Date Filing Date Title
CN201510293145.XA CN104828252A (en) 2015-06-02 2015-06-02 Method for implementing aerial continuous voyage for unmanned aerial vehicle

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Application Number Priority Date Filing Date Title
CN201510293145.XA CN104828252A (en) 2015-06-02 2015-06-02 Method for implementing aerial continuous voyage for unmanned aerial vehicle

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Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105068551A (en) * 2015-08-31 2015-11-18 深圳市飞研智能科技有限公司 Double-UAV control system with improvement of cruising ability
CN105270627A (en) * 2015-10-27 2016-01-27 深圳市飞研智能科技有限公司 Two-unmanned-aircraft system capable of being charged in air and improving endurance capability
CN105516254A (en) * 2015-11-26 2016-04-20 北京佰才邦技术有限公司 Data read-write method, device and system of unmanned device
WO2017035841A1 (en) * 2015-09-06 2017-03-09 深圳市大疆创新科技有限公司 Unmanned aerial vehicle and airborne supply method therefor, and floating platform and control method therefor
CN106779327A (en) * 2016-11-29 2017-05-31 国网山东省电力公司鄄城县供电公司 Device for electric power line patrol aircraft, aerocraft system and method
CN106998084A (en) * 2016-01-26 2017-08-01 丰唐物联技术(深圳)有限公司 Unmanned plane charging method and system
CN108028011A (en) * 2015-10-28 2018-05-11 松下知识产权经营株式会社 Use the observation system and observation procedure of flyer
CN110040012A (en) * 2019-04-22 2019-07-23 金陵科技学院 A kind of online charging method of unmanned plane receiving wireless charging based on multi-emitting list
CN111697559A (en) * 2020-07-16 2020-09-22 贵州梅岭电源有限公司 Space separable power supply system

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2000289695A (en) * 1999-04-06 2000-10-17 Hitachi Ltd Moored flight body and its utilizing system
US6422506B1 (en) * 2000-10-12 2002-07-23 The United States Of America As Represented By The Secretary Of The Navy Towed airborne array system
CN104029811A (en) * 2013-03-08 2014-09-10 波音公司 Autonomous Aircraft

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2000289695A (en) * 1999-04-06 2000-10-17 Hitachi Ltd Moored flight body and its utilizing system
US6422506B1 (en) * 2000-10-12 2002-07-23 The United States Of America As Represented By The Secretary Of The Navy Towed airborne array system
CN104029811A (en) * 2013-03-08 2014-09-10 波音公司 Autonomous Aircraft

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
中国科技网: "新西兰研发"空中充电"技术 将解决无人机续航问题", 《科技世界网》 *
李岳,张强,张灿: "无人机激光无线能量传输技术研究", 《飞航导弹》 *

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105068551B (en) * 2015-08-31 2018-04-24 深圳市飞研智能科技有限公司 A kind of double unmanned aerial vehicle control systems for lifting cruising ability
CN105068551A (en) * 2015-08-31 2015-11-18 深圳市飞研智能科技有限公司 Double-UAV control system with improvement of cruising ability
WO2017035841A1 (en) * 2015-09-06 2017-03-09 深圳市大疆创新科技有限公司 Unmanned aerial vehicle and airborne supply method therefor, and floating platform and control method therefor
CN107000849B (en) * 2015-09-06 2019-02-19 深圳市大疆创新科技有限公司 Unmanned plane and its air-supply method and floating platform and its control method
CN107000849A (en) * 2015-09-06 2017-08-01 深圳市大疆创新科技有限公司 Unmanned plane and its air-supply method and floating platform and its control method
CN105270627A (en) * 2015-10-27 2016-01-27 深圳市飞研智能科技有限公司 Two-unmanned-aircraft system capable of being charged in air and improving endurance capability
CN108028011A (en) * 2015-10-28 2018-05-11 松下知识产权经营株式会社 Use the observation system and observation procedure of flyer
CN105516254A (en) * 2015-11-26 2016-04-20 北京佰才邦技术有限公司 Data read-write method, device and system of unmanned device
WO2017129000A1 (en) * 2016-01-26 2017-08-03 丰唐物联技术(深圳)有限公司 Unmanned air vehicle charging method and system
CN106998084A (en) * 2016-01-26 2017-08-01 丰唐物联技术(深圳)有限公司 Unmanned plane charging method and system
CN106779327A (en) * 2016-11-29 2017-05-31 国网山东省电力公司鄄城县供电公司 Device for electric power line patrol aircraft, aerocraft system and method
CN106779327B (en) * 2016-11-29 2020-07-14 国网山东省电力公司鄄城县供电公司 Power line patrol aircraft, aircraft system and method
CN110040012A (en) * 2019-04-22 2019-07-23 金陵科技学院 A kind of online charging method of unmanned plane receiving wireless charging based on multi-emitting list
CN111697559A (en) * 2020-07-16 2020-09-22 贵州梅岭电源有限公司 Space separable power supply system

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Application publication date: 20150812