CN103532613A - Unmanned aerial vehicle remote task uploading system and method based on big dipper communication - Google Patents
Unmanned aerial vehicle remote task uploading system and method based on big dipper communication Download PDFInfo
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- CN103532613A CN103532613A CN201310500730.3A CN201310500730A CN103532613A CN 103532613 A CN103532613 A CN 103532613A CN 201310500730 A CN201310500730 A CN 201310500730A CN 103532613 A CN103532613 A CN 103532613A
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Abstract
The invention relates to the field of unmanned aerial vehicle and big dipper navigation communication, in particular to an unmanned aerial vehicle remote task uploading system and a method based on big dipper communication. The unmanned aerial vehicle remote task uploading system based on the big dipper communication comprises a ground monitoring system and an unmanned aerial vehicle flight control system, wherein the ground monitoring system comprises a first big dipper navigation communication module; the unmanned aerial vehicle flight control system comprises a second big dipper navigation communication module; the first big dipper navigation communication module is communicated with the second big dipper navigation communication module by a big dipper satellite navigation system; and flight mission information preset by the ground monitoring system is transmitted to the big dipper satellite navigation system by the first big dipper navigation communication module, and then sent to the second big dipper navigation communication module of the unmanned aerial vehicle flight control system by the big dipper satellite navigation system. The unmanned aerial vehicle remote task uploading system cannot be shielded by a terrain or a building easily, and is good in stability. With the adoption of the unmanned aerial vehicle remote task uploading system and the method based on the big dipper communication, unmanned aerial vehicle operation can be monitored effectively.
Description
Technical field
The present invention relates to unmanned plane, Big Dipper navigation communication field, relate in particular to unmanned plane remote task uploading system and method based on Big Dipper communication.
Background technology
Unmanned plane is a kind of not manned aircraft that utilizes radio robot and airborne flight control system to handle.Be widely used in the fields such as scouting, mapping.
Existing unmanned plane, at the scene of taking off, adopts data wire to upload aerial mission more.After aerial mission is uploaded, unmanned plane carries out operation by the aerial mission according to uploading.In operation process, need to change at any time aerial mission according to the situation of operation field, by radio robot is long-range, to unmanned plane, upload aerial mission changed information.
Yet, the transmission of ground wireless station is very easily subject to the restriction of blocking and being subject to transmission range of landform, building etc., when the operating environment complexity such as unmanned plane during flying is large to hypsography, forest regional, the communicating interrupt that may cause unmanned plane and radio robot, can not effectively monitor unmanned plane operation.
Summary of the invention
The object of the present invention is to provide a kind of unmanned plane remote task uploading system and method based on Big Dipper communication, to address the above problem.
A unmanned plane remote task uploading system for Big Dipper communication, comprises ground monitoring system and system for flight control computer; Ground monitoring system comprises the first Big Dipper navigation communication module; System for flight control computer comprises the second Big Dipper navigation communication module; The first Big Dipper navigation communication module and second Big Dipper navigation communication module are by Beidou satellite navigation system communication, for the default aerial mission information exchange of ground monitoring system being crossed to the first Big Dipper navigation communication module, be transferred to Beidou satellite navigation system, then by Beidou satellite navigation system, sent to the second Big Dipper navigation communication module of system for flight control computer.
The embodiment of the present invention also provides a kind of unmanned plane remote task method for uploading based on Big Dipper communication, comprises the steps:
The first Big Dipper navigation communication module is transferred to Beidou satellite navigation system by the default aerial mission modification information of ground monitoring system by the first Big Dipper navigation communication module;
By Beidou satellite navigation system, aerial mission modification information is sent to the second Big Dipper navigation communication module of system for flight control computer;
The second Big Dipper navigation communication module sends to system for flight control computer by aerial mission modification information.
Compared with prior art, the advantage of the embodiment of the present invention is: should unmanned plane remote task uploading system and method based on Big Dipper communication comprise ground monitoring system and system for flight control computer, wherein ground monitoring system is provided with the first Big Dipper navigation communication module, is provided with the second Big Dipper navigation communication module in system for flight control computer.Ground monitoring system is transferred to Beidou satellite navigation system by the first Big Dipper navigation communication module in the mode of short message by default aerial mission changed information, by Beidou satellite navigation system, sent to again the second Big Dipper navigation communication module of system for flight control computer, system for flight control computer receives after this aerial mission changed information, according to this aerial mission changed information renewal aerial mission and according to the aerial mission operation after upgrading.Short message mechanics of communication communication due to the communication employing Beidou satellite navigation system between ground monitoring system and system for flight control computer, this mechanics of communication is can be in China round-the-clock provides Communications service, be not vulnerable to blocking of landform, building, good stability.By this mechanics of communication, connect ground monitoring system and system for flight control computer, can effectively monitor unmanned plane operation.
Accompanying drawing explanation
Fig. 1 is the system schematic of the unmanned plane remote task uploading system based on Big Dipper communication of the embodiment of the present invention;
Fig. 2 is the flow chart of the unmanned plane remote task method for uploading based on Big Dipper communication of the embodiment of the present invention.
Embodiment
Below by specific embodiment, also by reference to the accompanying drawings the present invention is described in further detail.
As shown in Figure 1, the embodiment of the present invention provides a kind of unmanned plane remote task uploading system based on Big Dipper communication, comprises ground monitoring system 101 and system for flight control computer 107; Ground monitoring system 101 comprises the first Big Dipper navigation communication module 102; System for flight control computer 107 comprises the second Big Dipper navigation communication module 104; The default aerial mission modification information of ground monitoring system 101 is transferred to Beidou satellite navigation system 103 by the first Big Dipper navigation communication module 102, then by Beidou satellite navigation system 103, is sent to the second Big Dipper navigation communication module 104 of system for flight control computer 107.
This unmanned plane communication and control system comprises ground monitoring system 101 and system for flight control computer 107, wherein ground monitoring system 101 is provided with the first Big Dipper navigation communication module 102, is provided with the second Big Dipper navigation communication module 104 in system for flight control computer 107.Ground monitoring system 101 is transferred to Beidou satellite navigation system 103 by the first Big Dipper navigation communication module 102 in the mode of short message by default aerial mission changed information, by Beidou satellite navigation system 103, sent to again the second Big Dipper navigation communication module 104 of system for flight control computer, system for flight control computer 107 receives after this aerial mission changed information, according to this aerial mission changed information renewal aerial mission and according to the aerial mission operation after upgrading.Short message mechanics of communication communication due to the communication employing Beidou satellite navigation system between ground monitoring system 101 and system for flight control computer 107, this mechanics of communication is can be in China round-the-clock provides Communications service, be not vulnerable to landform, building blocks, good stability.By this mechanics of communication, connect ground monitoring system and system for flight control computer, can effectively control unmanned plane operation.
In addition, because adopting Beidou satellite navigation system, unmanned plane realizes the transmission of information between unmanned plane and ground monitoring system, the second Big Dipper navigation communication module 104 is installed on unmanned plane, and this module volume is little, lightweight, cost is low, is suitable for normal domestic unmanned plane.Wherein, aerial mission modification information comprises flight path information, route information, exposure point position information, aerial conductor information, jump area dot information.For example, in unmanned plane operation process, in the time of need to changing the flight path of unmanned plane, ground monitoring system is made after the flight path after change according to the digital elevation model dem data of operating area, this flight path is encrypted to packing and by the first Big Dipper navigation communication module, with short message mechanics of communication, send to Beidou satellite navigation system, Beidou satellite navigation system sends to this flight path the second communication module mating with the first Big Dipper communication module again, realizes uploading in real time of flight path.
In order to ensure unmanned plane, according to predetermined flight path flight, system for flight control computer also comprises single-frequency GPS module 105 and processor 108; Single-frequency GPS module 105 is connected with processor 108, combines and resolves, for unmanned plane provides navigation information for the GPS navigation information receiving being sent to processor 108.Wherein single-frequency GPS module comprises the single-frequency GPS processing unit being integrated in flight control system and is positioned at the single-frequency GPS antenna outside unmanned plane.
In order to ensure stablizing of unmanned plane during flying attitude, system for flight control computer also comprises IMU module 106; IMU module 106 is connected with processor 108,, for the acceleration receiving and angular velocity information being sent to processor 108, combine and resolve, for unmanned plane provides attitude information.
Further, system for flight control computer also comprises pitot 110; Pitot 110 is electrically connected to processor 108, for air velocity, the atmospheric pressure that detection is obtained, sends to processor, for unmanned plane provides air speed and pressure altitude.
Further, system for flight control computer also comprises camera and The Cloud Terrace, possesses the function of controlling camera exposure and cradle head control; Camera and The Cloud Terrace are electrically connected to processor respectively; System for flight control computer sends exposed pulse and controls camera exposure, and The Cloud Terrace is used for making camera to keep taking straight down.When aspect changes, The Cloud Terrace is adjusted in time, and camera is kept straight down.For example, when unmanned plane luffing angle or roll angle change, the adjusting mechanism carrying in The Cloud Terrace is adjusted the angle of camera automatically, makes camera in shooting angle straight down.When the yaw angle of unmanned plane changes, Inertial Measurement Unit detects the yaw angle information of unmanned plane and this information is sent to processor, processor obtains The Cloud Terrace according to this yaw angle information and adjusts instruction and this The Cloud Terrace adjustment instruction is sent to The Cloud Terrace, The Cloud Terrace adjusts according to this The Cloud Terrace the angle that The Cloud Terrace is adjusted in instruction, makes camera keep shooting angle straight down.
Wherein, system for flight control computer also comprises memory 109; Memory 109 is electrically connected to processor 108, for storing the flight parameter of unmanned plane.Be that any information that unmanned plane obtains all can be stored in this memory.
The embodiment of the present invention also provides a kind of unmanned plane remote task method for uploading based on Big Dipper communication that uses above-mentioned uploading system, as shown in Figure 2, comprises the steps:
S201, the first Big Dipper navigation communication module is transferred to Beidou satellite navigation system by the default aerial mission modification information of ground monitoring system by the first Big Dipper navigation communication module;
S202, is sent to aerial mission modification information by Beidou satellite navigation system the second Big Dipper navigation communication module of system for flight control computer;
S203, the second Big Dipper navigation communication module sends to system for flight control computer by aerial mission modification information.
The foregoing is only the preferred embodiments of the present invention, be not limited to the present invention, for a person skilled in the art, the present invention can have various modifications and variations.Within the spirit and principles in the present invention all, any modification of doing, be equal to replacement, improvement etc., within all should being included in protection scope of the present invention.
Claims (8)
1. the unmanned plane remote task uploading system based on Big Dipper communication, is characterized in that, comprises ground monitoring system and system for flight control computer;
Described ground monitoring system comprises the first Big Dipper navigation communication module; Described system for flight control computer comprises the second Big Dipper navigation communication module; Described the first Big Dipper navigation communication module and described the second Big Dipper navigation communication module are by Beidou satellite navigation system communication, for the default aerial mission modification information of described ground monitoring system is transferred to Beidou satellite navigation system by described the first Big Dipper navigation communication module, then by Beidou satellite navigation system, sent to the second Big Dipper navigation communication module of described system for flight control computer.
2. the unmanned plane remote task uploading system based on Big Dipper communication as claimed in claim 1, is characterized in that, described aerial mission modification information comprises flight path information, route information, exposure point position information, aerial conductor information, jump area dot information etc.
3. the unmanned plane remote task uploading system based on Big Dipper communication as claimed in claim 2, is characterized in that, described system for flight control computer also comprises single-frequency GPS module and processor;
Described single-frequency GPS module is connected with described processor, combines and resolves, for unmanned plane provides navigation information for the GPS navigation information receiving being sent to described processor.
4. the unmanned plane remote task uploading system based on Big Dipper communication as claimed in claim 3, is characterized in that, described system for flight control computer also comprises IMU module;
Described IMU module is connected with described processor, combines and resolves, for described unmanned plane provides attitude information for the acceleration receiving and angular velocity information being sent to described processor.
5. the unmanned plane remote task uploading system based on Big Dipper communication as claimed in claim 4, is characterized in that, described system for flight control computer also comprises pitot;
Described pitot is electrically connected to described processor, for air velocity, the atmospheric pressure that detection is obtained, sends to described processor, for unmanned plane provides air speed and pressure altitude.
6. the unmanned plane remote task uploading system based on Big Dipper communication as claimed in claim 5, is characterized in that, described system for flight control computer also comprises camera and The Cloud Terrace;
Described camera and described The Cloud Terrace are electrically connected to described processor respectively; Described system for flight control computer is controlled camera exposure, and described The Cloud Terrace is for making described camera keep shooting angle straight down.
7. the unmanned plane remote task uploading system based on Big Dipper communication as claimed in claim 6, is characterized in that, also comprises memory;
Described memory is connected with described processor, for storing the flight parameter of unmanned plane.
8. a method for uploading for the unmanned plane remote task uploading system based on Big Dipper communication of use as described in any one in claim 1-7, is characterized in that, comprises the steps:
The first Big Dipper navigation communication module is transferred to Beidou satellite navigation system by the default aerial mission modification information of ground monitoring system by described the first Big Dipper navigation communication module;
By Beidou satellite navigation system, described aerial mission modification information is sent to the second Big Dipper navigation communication module of system for flight control computer;
Described the second Big Dipper navigation communication module sends to described system for flight control computer by described aerial mission modification information.
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Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104615143A (en) * | 2015-01-23 | 2015-05-13 | 广州快飞计算机科技有限公司 | Unmanned aerial vehicle scheduling method |
CN105243877A (en) * | 2015-10-18 | 2016-01-13 | 上海圣尧智能科技有限公司 | Unmanned plane air traffic control module and the unmanned plane |
CN105373132A (en) * | 2015-11-26 | 2016-03-02 | 北京浩恒征途航空科技有限公司 | Low-altitude remote sensing system based on automatic cruise unmanned aerial vehicle and remote sensing method thereof |
CN105511489A (en) * | 2015-12-07 | 2016-04-20 | 中国电子科技集团公司第十研究所 | Multi-aircraft configuration terminal capable of being quickly accessed to Big Dipper constellation phased-array inter-satellite link |
CN106291620A (en) * | 2016-08-16 | 2017-01-04 | 广东容祺智能科技有限公司 | A kind of location tracking being applied to unmanned plane and flying quality storage system |
CN106291638A (en) * | 2016-08-16 | 2017-01-04 | 广东容祺智能科技有限公司 | A kind of unmanned plane dual link tracing system of integrated black box |
CN107295811A (en) * | 2016-07-05 | 2017-10-24 | 深圳市大疆创新科技有限公司 | A kind of method and device for checking of networking |
CN107302394A (en) * | 2017-06-19 | 2017-10-27 | 四川腾盾科技有限公司 | A kind of unmanned aerial vehicle (UAV) control method based on Big Dipper short message |
CN108718112A (en) * | 2018-07-17 | 2018-10-30 | 易讯科技股份有限公司 | A kind of grid monitoring system and method based on triones navigation system |
CN109143284A (en) * | 2018-08-29 | 2019-01-04 | 东莞市普灵思智能电子有限公司 | A kind of embedded Beidou GPS positioning system and localization method |
CN109194385A (en) * | 2018-10-31 | 2019-01-11 | 中国船舶工业系统工程研究院 | Unmanned surface vehicle long-range control method based on Big Dipper short message |
CN112099524A (en) * | 2020-08-21 | 2020-12-18 | 太仓云路遥智能科技有限公司 | Unmanned aerial vehicle navigation positioning integrated management system based on three-dimensional 5G networking |
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Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201788592U (en) * | 2010-09-07 | 2011-04-06 | 四川信通通信技术开发有限责任公司 | Real-time positioning monitoring management system of unmanned aerial vehicle |
CN102211670A (en) * | 2011-05-17 | 2011-10-12 | 云南电网公司普洱供电局 | Fixed-wing unmanned plane fixed-point shooting system and method for troubleshooting transmission lines thereof |
KR20130009895A (en) * | 2013-01-05 | 2013-01-23 | 이상윤 | Unmanned aeriel vehicle network system with spatial information technology |
-
2013
- 2013-10-22 CN CN201310500730.3A patent/CN103532613A/en active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201788592U (en) * | 2010-09-07 | 2011-04-06 | 四川信通通信技术开发有限责任公司 | Real-time positioning monitoring management system of unmanned aerial vehicle |
CN102211670A (en) * | 2011-05-17 | 2011-10-12 | 云南电网公司普洱供电局 | Fixed-wing unmanned plane fixed-point shooting system and method for troubleshooting transmission lines thereof |
KR20130009895A (en) * | 2013-01-05 | 2013-01-23 | 이상윤 | Unmanned aeriel vehicle network system with spatial information technology |
Non-Patent Citations (1)
Title |
---|
宫磊: ""基于北斗卫星导航定位系统的测控应用"", 《2007年中国浮空器大会论文集》, 24 July 2008 (2008-07-24) * |
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CN104615143A (en) * | 2015-01-23 | 2015-05-13 | 广州快飞计算机科技有限公司 | Unmanned aerial vehicle scheduling method |
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CN105373132A (en) * | 2015-11-26 | 2016-03-02 | 北京浩恒征途航空科技有限公司 | Low-altitude remote sensing system based on automatic cruise unmanned aerial vehicle and remote sensing method thereof |
CN105511489A (en) * | 2015-12-07 | 2016-04-20 | 中国电子科技集团公司第十研究所 | Multi-aircraft configuration terminal capable of being quickly accessed to Big Dipper constellation phased-array inter-satellite link |
CN105511489B (en) * | 2015-12-07 | 2018-05-22 | 中国电子科技集团公司第十研究所 | Quickly access the multi-aircraft configurating terminal of Big Dipper constellation phased array inter-satellite link |
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CN107295811A (en) * | 2016-07-05 | 2017-10-24 | 深圳市大疆创新科技有限公司 | A kind of method and device for checking of networking |
US11104435B2 (en) | 2016-07-05 | 2021-08-31 | SZ DJI Technology Co., Ltd. | Verification method and apparatus |
CN106291620A (en) * | 2016-08-16 | 2017-01-04 | 广东容祺智能科技有限公司 | A kind of location tracking being applied to unmanned plane and flying quality storage system |
CN106291638A (en) * | 2016-08-16 | 2017-01-04 | 广东容祺智能科技有限公司 | A kind of unmanned plane dual link tracing system of integrated black box |
CN107302394A (en) * | 2017-06-19 | 2017-10-27 | 四川腾盾科技有限公司 | A kind of unmanned aerial vehicle (UAV) control method based on Big Dipper short message |
CN108718112A (en) * | 2018-07-17 | 2018-10-30 | 易讯科技股份有限公司 | A kind of grid monitoring system and method based on triones navigation system |
CN109143284A (en) * | 2018-08-29 | 2019-01-04 | 东莞市普灵思智能电子有限公司 | A kind of embedded Beidou GPS positioning system and localization method |
CN109194385A (en) * | 2018-10-31 | 2019-01-11 | 中国船舶工业系统工程研究院 | Unmanned surface vehicle long-range control method based on Big Dipper short message |
CN112099524A (en) * | 2020-08-21 | 2020-12-18 | 太仓云路遥智能科技有限公司 | Unmanned aerial vehicle navigation positioning integrated management system based on three-dimensional 5G networking |
CN113067624A (en) * | 2021-03-15 | 2021-07-02 | 陕西北斗金箭航空科技有限公司 | Unmanned aerial vehicle control method based on Beidou message chain |
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