CN104803009A - Unmanned aerial vehicle (UAV) ground comprehensive detection system and UAV ground comprehensive detection method - Google Patents
Unmanned aerial vehicle (UAV) ground comprehensive detection system and UAV ground comprehensive detection method Download PDFInfo
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Abstract
The invention provides an unmanned aerial vehicle (UAV) ground comprehensive detection system and a UAV ground comprehensive detection method, belonging to the field of UAV data processing. The UAV ground comprehensive detection system comprises a main program module, an electromechanical system detection module, a system parameter binding module, a system failure download and record module, a communication interface module, a power device detection module and a vehicle management system detection module, wherein all the modules, except the main program module, are independent of one another, and are respectively connected with the main program module; the UAV ground comprehensive detection system is also provided with data buses which are respectively connected with corresponding data bus interfaces of a UAV, so that data exchange is realized, and the UAV is detected. After the UAV ground comprehensive detection system and the UAV ground comprehensive detection method are used for detecting an aircraft, multiple detection devices prepared by preflight maintenance in the prior art can be replaced, so that maintenance devices are reduced, the maintenance cost is lowered, the complicated operation of the multiple devices is avoided, the preflight preparation time of the aircraft is effectively shortened, and the information interaction with a complicated airborne system is realized.
Description
Technical field
The present invention relates to Unmanned Aerial Vehicle Data process field, particularly relate to a kind of unmanned aerial vehicle comprehensive detection system and method.
Background technology
China can't realize the total system comprehensive detection of complicated unmanned plane machine system at present for the surface detection technique of unmanned plane.The mode that pre-flight detection adopts each system to detect respectively usually completes, and required check implement quantity is many, and before flight, setup time is long, and can not meet the requirement of the quick preparation of mobile system before unmanned plane during flying, system development cost also increases thereupon.
Summary of the invention
The first object of the present invention is to solve above-mentioned deficiency of the prior art, a kind of unmanned aerial vehicle method for comprehensive detection is provided, reduce maintenance equipment, reduce maintenance cost, avoid multiple devices complex operation complicated situation, effective time shortening front preparation of flying, the demand of quick preparation before meeting unmanned aerial vehicle flight.
The first object of the present invention realizes a kind of unmanned aerial vehicle comprehensive detection system by following scheme, for Unmanned Aerial Vehicle Data process, comprising:
Main program module, for system startup, initialization and dispatch other modules;
Mechatronic Systems detection module, for showing power supply, electromechanics, fuel oil system state, the control commands such as electrical generator, fuel charger, fule shut-off valve send, and Autonomous test instruction sends;
System parameter bookbinding module, for the bookbinding of receive navigation parameters, course data, atmospheric parameter;
The system failure is downloaded and logging modle, for the inquiry of the system failure, download, record and playback;
Communication interface module, completes the packing of data, parsing, reception, transmission according to the data frame format of regulation;
Engine installation detection module, engine condition display, inquiry, the control command of engine starting, Throttle Opening Control, patten transformation, maintenance sends, and Autonomous test instruction sends,
It is separate and be connected with main program module separately and carry out data exchange between above-mentioned each system other modules except main program module,
Also be provided with data bus to be connected with Unmanned Aerial Vehicle Data bus interface.
In such scheme preferably, described data bus is the data frame format of RS422/GJB289/ARINC429/ analog quantity/measures of dispersion according to interactive form.
The second object of the present invention is to provide a kind of unmanned aerial vehicle method for comprehensive detection, instead of conventional airplane take off before the multinomial check implement for preparing of engineering, decrease maintenance equipment, reduce maintenance cost, avoid multiple devices complex operation complicated.
The second object of the present invention is achieved through the following technical solutions:
A kind of unmanned aerial vehicle method for comprehensive detection, adopts the unmanned aerial vehicle comprehensive detection system described in such scheme, comprises the following steps:
S1: unmanned aerial vehicle comprehensive detection system is connected with Unmanned Aerial Vehicle Data bus interface by data bus;
S2: start unmanned aerial vehicle comprehensive detection system and unmanned aerial vehicle computer management system;
S3: key in up-on command at unmanned aerial vehicle comprehensive detection system and send to unmanned aerial vehicle computer management system;
S4: the unmanned aerial vehicle comprehensive detection system up-on command of reception is sent to corresponding unmanned aerial vehicle onboard equipment by Logic judgment corresponding instruction by unmanned aerial vehicle computer management system;
S5: airborne equipment receives corresponding instruction and carries out Autonomous test;
S6: Autonomous test result is back to unmanned aerial vehicle computer management system by airborne equipment;
S7: Autonomous test result is sent to unmanned aerial vehicle comprehensive detection system by data bus by unmanned aerial vehicle computer management system;
S8: unmanned aerial vehicle comprehensive detection system is received from testing result and carries out Data Analysis and is presented on unmanned aerial vehicle comprehensive detection system interface.
In such scheme preferably, the Detection task that checking system performs comprises Mechatronic Systems comprehensive detection, aircraft management detects, engine installation detects and interface detects.
Usefulness of the present invention is: use unmanned aerial vehicle comprehensive detection system provided by the invention and method to carry out Comprehensive detection to complicated Unmanned Aircraft Systems (UAS), the time prepared before effectively shortening flight, the demand prepared fast before meeting unmanned aerial vehicle flight, there is higher portability, reduce development cost, shorten the lead time.
Accompanying drawing explanation
Fig. 1 is the schematic diagram of the preferred embodiment according to unmanned aerial vehicle method for comprehensive detection of the present invention.
Detailed description of the invention
Below in conjunction with accompanying drawing, unmanned aerial vehicle comprehensive detection system provided by the invention and method are described in further details.
A unmanned aerial vehicle comprehensive detection system as shown in Figure 1, for Unmanned Aerial Vehicle Data process, comprising:
Main program module, for system startup, initialization and dispatch other modules; Mechatronic Systems detection module, for showing power supply, electromechanics, fuel oil system state, the control commands such as electrical generator, fuel charger, fule shut-off valve send, and Autonomous test instruction sends; System parameter bookbinding module, for the bookbinding of receive navigation parameters, course data, atmospheric parameter; The system failure is downloaded and logging modle, for the inquiry of the system failure, download, record and playback; Communication interface module, completes the packing of data, parsing, reception, transmission according to the data frame format of regulation; Engine installation detection module, engine condition display, inquiry, the control command of engine starting, Throttle Opening Control, patten transformation, maintenance sends, and Autonomous test instruction sends.Separate and be connected with main program module separately and carry out data exchange between each system other modules except main program module, be also provided with data bus and be connected with Unmanned Aerial Vehicle Data bus interface.
Be directed to the feature that mobile system is complicated, cross-linked form is various of existing unmanned plane, data bus interface design is become the Frame definition format being applicable to the tens of kinds of data interaction forms such as RS422, GJB289, ARINC429, analog quantity, discrete magnitude by unmanned aerial vehicle comprehensive detection system provided by the invention, multiplexing and the instruction target distribution technology by Frame, reduce the complexity of mobile system design, achieve the information interaction with complicated mobile system; Shown in table 1 is unmanned aerial vehicle comprehensive detection system conventional data command frame concrete structure; A table 2 ground inspection operation conventional data order returns frame concrete structure.
Table 1 ground inspection operation conventional data command frame structure
Unmanned aerial vehicle comprehensive detection system provided by the invention devises the actuating logic of crucial complex command, realizes maximization and the exact failure location of instruction efficiency, solves the self-monitoring difficult problem of full machine dozens of systematic collaboration; By designing a key traversal queries instruction, achieve a key control of mobile system Autonomous test, status poll, systemic-function contains 100 multinomial instructions and more than 400 state display, before making flight, preparation form becomes full automatic control from original multinomial Non-follow control fast, improves degree of automation and the work efficiency of systems axiol-ogy.Contain much information for mobile system, complicated operation and the high feature of security requirement, carried out ergonomic's optimal design and safety Design, have employed chain design safety safety method and page info vision optimal design.
Unmanned aerial vehicle method for comprehensive detection provided by the invention comprises the steps:
S1: unmanned aerial vehicle comprehensive detection system is connected with Unmanned Aerial Vehicle Data bus interface by data bus;
S2: start unmanned aerial vehicle comprehensive detection system and unmanned aerial vehicle computer management system;
S3: key in up-on command at unmanned aerial vehicle comprehensive detection system and send to unmanned aerial vehicle computer management system;
S4: the unmanned aerial vehicle comprehensive detection system up-on command of reception is sent to corresponding unmanned aerial vehicle onboard equipment by Logic judgment corresponding instruction by unmanned aerial vehicle computer management system;
S5: airborne equipment receives corresponding instruction and carries out Autonomous test;
S6: Autonomous test result is back to unmanned aerial vehicle computer management system by airborne equipment;
S7: Autonomous test result is sent to unmanned aerial vehicle comprehensive detection system by data bus by unmanned aerial vehicle computer management system;
S8: unmanned aerial vehicle comprehensive detection system is received from testing result and carries out Data Analysis and is presented on unmanned aerial vehicle comprehensive detection system interface.
In concrete use procedure, adopt unmanned aerial vehicle comprehensive detection system provided by the invention and method to the operation of unmanned plane Throttle Opening Control, throttle size is set in unmanned aerial vehicle comprehensive detection system provided by the invention and enables sensing button, system fills in corresponding uplink frame data by the mode of message trigger and according to throttle with fly pipe communication interface and fill in throttle and arrange uplink frame in data content, throttle is arranged instruction to be sent to by RS422 bus and fly pipe computer system, fly pipe computer system the communication frames of data content portion is extracted directly to be transmitted to engine installation control terminal, corresponding operation is performed by engine installation control terminal.
The transmission of fule shut-off valve instruction.Unmanned aerial vehicle comprehensive detection system provided by the invention is clicked and opens fule shut-off valve instruction, system obtains message trigger, concurrent serve row frame data and fill in walk-off-mode analog quantity instruction is set accordingly, data uplink frame is sent to by RS422 bus and flies pipe computing machine, fly pipe computing machine and perform corresponding operation by rigid line voltage signal control convenience.If wherein there is fault, in unmanned aerial vehicle comprehensive detection system provided by the invention, failure message record is also preserved with unmanned aerial vehicle comprehensive detection system by system failure download and logging modle, pending fault re-starts aforesaid operations after getting rid of, until operation completes smoothly, no longer include malfunction coefficient.
Walk-off-mode analog quantity is monitored.The data acquisition of walk-off-mode analog quantity is by the walk-off-mode analog quantity signal voltage flying pipe computer acquisition equipment and provide, convert binary mode to and fill in into Frame and be sent to unmanned aerial vehicle comprehensive detection system provided by the invention by flying pipe computing machine by RS422 bus, unmanned aerial vehicle comprehensive detection system is resolved after receiving the data of aircraft computer management system, data is shown in unmanned aerial vehicle comprehensive detection system.
Information inquiry.After ground inspection sends query statement, software transfer data communication module obtains the data flying pipe and hand down, and software inhouse calling data resolves distribution module, data is resolved, the Data dissemination of having resolved is carried out data display update to corresponding display interface.
More than be described in detail in conjunction with specific embodiments of the invention, but be not limitation of the present invention, such as invent the unmanned aerial vehicle comprehensive detection system that provides and method data connect from bus data frame format, data bus the sequencing etc. started with system, everyly according to technical spirit of the present invention, technical scope of the present invention is all belonged to any simple modification made for any of the above embodiments, also it should be noted that, comprise the combination in any between each part mentioned above according to the category of unmanned aerial vehicle comprehensive detection system of the present invention and method and technology scheme.
Claims (4)
1. a unmanned aerial vehicle comprehensive detection system, for Unmanned Aerial Vehicle Data process, is characterized in that, comprising:
Main program module, for system startup, initialization and dispatch other modules;
Mechatronic Systems detection module, for showing power supply, electromechanics, fuel oil system state, the control commands such as electrical generator, fuel charger, fule shut-off valve send, and Autonomous test instruction sends;
System parameter bookbinding module, for the bookbinding of receive navigation parameters, course data, atmospheric parameter;
The system failure is downloaded and logging modle, for the inquiry of the system failure, download, record and playback;
Communication interface module, completes the packing of data, parsing, reception, transmission according to the data frame format of regulation;
Engine installation detection module, engine condition display, inquiry, the control command of engine starting, Throttle Opening Control, patten transformation, maintenance sends, and Autonomous test instruction sends,
It is separate and be connected with main program module separately and carry out data exchange between above-mentioned each system other modules except main program module,
Also be provided with data bus to be connected with Unmanned Aerial Vehicle Data bus interface.
2. unmanned aerial vehicle comprehensive detection system as claimed in claim 1, is characterized in that: described data bus is the data frame format of RS422/GJB289/ARINC429/ analog quantity/measures of dispersion according to interactive form.
3. a unmanned aerial vehicle method for comprehensive detection, is characterized in that, adopts unmanned aerial vehicle comprehensive detection system as claimed in claim 1, comprises the following steps:
S1: unmanned aerial vehicle comprehensive detection system is connected with Unmanned Aerial Vehicle Data bus interface by data bus;
S2: start unmanned aerial vehicle comprehensive detection system and unmanned aerial vehicle computer management system;
S3: key in up-on command at unmanned aerial vehicle comprehensive detection system and send to unmanned aerial vehicle computer management system;
S4: the unmanned aerial vehicle comprehensive detection system up-on command of reception is sent to corresponding unmanned aerial vehicle onboard equipment by Logic judgment corresponding instruction by unmanned aerial vehicle computer management system;
S5: airborne equipment receives corresponding instruction and carries out Autonomous test;
S6: Autonomous test result is back to unmanned aerial vehicle computer management system by airborne equipment;
S7: Autonomous test result is sent to unmanned aerial vehicle comprehensive detection system by data bus by unmanned aerial vehicle computer management system;
S8: unmanned aerial vehicle comprehensive detection system is received from testing result and carries out Data Analysis and is presented on unmanned aerial vehicle comprehensive detection system interface.
4. unmanned aerial vehicle method for comprehensive detection according to claim 3, is characterized in that: the Detection task that described checking system performs comprises Mechatronic Systems comprehensive detection, aircraft management detects, engine installation detects and interface detects.
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105204329A (en) * | 2015-11-05 | 2015-12-30 | 北京精航科技有限公司 | Preflight sound control equipment checking method and system for unmanned aerial vehicle |
| CN105644775A (en) * | 2016-03-16 | 2016-06-08 | 中国直升机设计研究所 | Flight test command and control system for unmanned helicopters |
| CN105857637A (en) * | 2016-06-08 | 2016-08-17 | 广东容祺智能科技有限公司 | Unmanned aerial vehicle self-checking system |
| CN105911979A (en) * | 2016-05-31 | 2016-08-31 | 中国航空工业集团公司西安飞机设计研究所 | Flight bus data processing method |
| CN105974222A (en) * | 2016-04-27 | 2016-09-28 | 乐视控股（北京）有限公司 | Unmanned aerial vehicle fault detection method, apparatus and system thereof |
| CN106428619A (en) * | 2015-08-07 | 2017-02-22 | 中国电力科学研究院 | Performance detection method of unmanned aircraft for power transmission line |
| CN107517076A (en) * | 2017-07-25 | 2017-12-26 | 中国南方航空股份有限公司 | One kind is based on event driven Data-Link uplink triggering device and its triggering method |
| WO2018010130A1 (en) * | 2016-07-14 | 2018-01-18 | SZ DJI Technology Co., Ltd. | Programmable motor controller using a motor |
| CN108196531A (en) * | 2018-01-31 | 2018-06-22 | 佛山市神风航空科技有限公司 | A kind of sampling unmanned plane failure based reminding method and device |
| CN108254208A (en) * | 2018-01-12 | 2018-07-06 | 中国航空工业集团公司北京长城航空测控技术研究所 | A kind of simulator data creation method for aircraft complete machine test stand |
| CN108255149A (en) * | 2017-12-08 | 2018-07-06 | 中国航空工业集团公司成都飞机设计研究所 | It is a kind of to be remotely controlled the method that unmanned plane flies guard system failure of removing |
| CN108910077A (en) * | 2018-05-31 | 2018-11-30 | 深圳市易飞方达科技有限公司 | Online test method before unmanned plane flies |
| CN109110154A (en) * | 2018-08-30 | 2019-01-01 | 芜湖翼讯飞行智能装备有限公司 | A kind of self checking method and its auxiliary device of automatic unmanned plane |
| CN109956050A (en) * | 2019-02-21 | 2019-07-02 | 顺丰科技有限公司 | Unmanned plane during flying detects instruction device, method, system and unmanned plane |
| CN110027729A (en) * | 2019-05-09 | 2019-07-19 | 西北工业大学 | A kind of Unmanned Aerial Vehicle Powerplants system rapid detection method |
| CN110132602A (en) * | 2019-05-10 | 2019-08-16 | 西北工业大学 | A kind of Unmanned Aerial Vehicle Powerplants system ground detector |
| CN110658835A (en) * | 2019-09-19 | 2020-01-07 | 中国航空无线电电子研究所 | Unmanned aerial vehicle flight control method and system |
| CN111191325A (en) * | 2019-12-24 | 2020-05-22 | 中国航空工业集团公司西安飞机设计研究所 | Aircraft direct flight preparation modeling method based on SysML |
| CN111402863A (en) * | 2020-03-23 | 2020-07-10 | 北京京东乾石科技有限公司 | Control method, system, device, medium and equipment for formation unmanned aerial vehicle |
| CN112115552A (en) * | 2020-09-16 | 2020-12-22 | 天津津航计算技术研究所 | Airborne flight data recharging method and device |
| CN113467278A (en) * | 2021-05-24 | 2021-10-01 | 中国航空工业集团公司沈阳飞机设计研究所 | Man-machine interaction terminal for ground maintenance of airborne power system |
| CN113650806A (en) * | 2021-10-21 | 2021-11-16 | 西安羚控电子科技有限公司 | Ground detection system and method for unmanned aerial vehicle |
| CN113693051A (en) * | 2018-12-10 | 2021-11-26 | 拜耳公司 | Spray vehicle |
| CN113741547A (en) * | 2021-10-14 | 2021-12-03 | 广东汇天航空航天科技有限公司 | Aircraft power equipment self-checking method, device and system and aircraft |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201698228U (en) * | 2010-06-12 | 2011-01-05 | 北京国科环宇空间技术有限公司 | Equipment supervisor in aircraft and health supervisor in equipment supervisor |
| CN102030111A (en) * | 2010-11-16 | 2011-04-27 | 中国民航大学 | Aircraft CFDS (Centralized Fault Display System) data analyzer and implementation method thereof |
| CN102799175A (en) * | 2012-08-17 | 2012-11-28 | 中国航天时代电子公司 | Rapid detection device and detection method for unmanned aircraft system |
| EP2581796A1 (en) * | 2011-10-14 | 2013-04-17 | Honeywell International Inc. | Method and computer readable storage media for distributed diagnostic reasoning |
| US20140012461A1 (en) * | 2012-07-04 | 2014-01-09 | Alenia Aermacchi S.P.A. | Method for performing diagnostics of a structure subject to loads and system for implementing said method |
| CN103558838A (en) * | 2013-11-01 | 2014-02-05 | 北京航空航天大学 | Solid-liquid power air vehicle ground test and launch control system of 422 bus |
-
2015
- 2015-04-27 CN CN201510211508.0A patent/CN104803009A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201698228U (en) * | 2010-06-12 | 2011-01-05 | 北京国科环宇空间技术有限公司 | Equipment supervisor in aircraft and health supervisor in equipment supervisor |
| CN102030111A (en) * | 2010-11-16 | 2011-04-27 | 中国民航大学 | Aircraft CFDS (Centralized Fault Display System) data analyzer and implementation method thereof |
| EP2581796A1 (en) * | 2011-10-14 | 2013-04-17 | Honeywell International Inc. | Method and computer readable storage media for distributed diagnostic reasoning |
| US20140012461A1 (en) * | 2012-07-04 | 2014-01-09 | Alenia Aermacchi S.P.A. | Method for performing diagnostics of a structure subject to loads and system for implementing said method |
| CN102799175A (en) * | 2012-08-17 | 2012-11-28 | 中国航天时代电子公司 | Rapid detection device and detection method for unmanned aircraft system |
| CN103558838A (en) * | 2013-11-01 | 2014-02-05 | 北京航空航天大学 | Solid-liquid power air vehicle ground test and launch control system of 422 bus |
Non-Patent Citations (2)
| Title |
|---|
| 张朋等: "基于PAWS的预警机机载设备综合自动测试系统设计", 《测控技术》 * |
| 路蔼梅等: "一种无人机通用综合检测系统", 《北京航空航天大学学报》 * |
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| CN112115552B (en) * | 2020-09-16 | 2022-10-25 | 天津津航计算技术研究所 | Airborne flight data recharging method and device |
| CN113467278A (en) * | 2021-05-24 | 2021-10-01 | 中国航空工业集团公司沈阳飞机设计研究所 | Man-machine interaction terminal for ground maintenance of airborne power system |
| CN113741547A (en) * | 2021-10-14 | 2021-12-03 | 广东汇天航空航天科技有限公司 | Aircraft power equipment self-checking method, device and system and aircraft |
| CN113650806A (en) * | 2021-10-21 | 2021-11-16 | 西安羚控电子科技有限公司 | Ground detection system and method for unmanned aerial vehicle |
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