CN202533754U - Ground monitoring system for unmanned vehicle physical simulated test platform - Google Patents
Ground monitoring system for unmanned vehicle physical simulated test platform Download PDFInfo
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- CN202533754U CN202533754U CN2011203890986U CN201120389098U CN202533754U CN 202533754 U CN202533754 U CN 202533754U CN 2011203890986 U CN2011203890986 U CN 2011203890986U CN 201120389098 U CN201120389098 U CN 201120389098U CN 202533754 U CN202533754 U CN 202533754U
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Abstract
The utility model provides a ground monitoring system for an unmanned aerial vehicle physical simulated test platform. The ground monitoring system comprises: an industrial control computer with three screens, and a manual driving mechanism, a power supply, a data transmission radio which communicates with an airborne test system through a data link, and a first display screen to a third display screen. The manual driving mechanism, the power supply, the data transmission radio, and the first display screen to the third display screen are connected with the industrial control computer with three screens. The ground monitoring system is also provided with a manual controller which communicates with the airborne test system through a second data link. The ground monitoring system has a high and concise integrated level, and is stable in operation, timely and continuous in collecting data, thereby being beneficial to a physical simulated test. And data of the finished test is automatically recorded, so that ground station staff's work load is reduced. The ground monitoring system enables intuitive and reliable evaluation for a flight control system control algorithm.
Description
Technical field
The utility model relates to a kind of simulation test platform.Particularly relate to a kind of unmanned vehicle physical simulation test platform ground monitoring system that can realize and reliable assessment directly perceived to the flight control system control algolithm.
Background technology
In recent years, the research of UAV Flight Control has been become a focus in control field.Some unmanned vehicle control algolithms have appearred thereupon; Checking to these control algolithm validity and accuracy; Often carry out final inspection through practical flight device Live Flying; This brings certain potential safety hazard just for practical flight device flight test, and often need spend more time, manpower, financial resources to effective assessment of algorithm.At present, in order to address these problems, ground mathematical simulation and HWIL simulation test are adopted in the assessment of these algorithms usually.These two kinds of methods all are subject to modeling technique level and physical environment emulation level to a certain extent, and its simulation result and real system have bigger deviation.The unmanned aerial vehicle control station is the important component part of UAS, is the basic guarantee that realizes that UAS debugging and reliability are used, and its human-computer interaction interface that provides can make unmanned plane in the process of executing the task, give full play to people's subjective dynamic role.
Traditional unmanned vehicle ground monitoring system mainly can be accomplished real-time collection, analyze telemetry, and the timed sending telecommand shows the function of flying quality in real time.This ground control station system is when assessing control algolithm; In test of boat appearance and navigational guidance test, can not give expression to the difference under true attitude and ship trajectory and the perfect condition intuitively, thereby can not well carry out directly perceived and assessment reliably control algolithm.
Summary of the invention
The utility model technical matters to be solved is; Providing a kind of can gather in flight course in the parameters of unmanned vehicle physical model in real time, offers the personnel's of land station unmanned vehicle physical simulation test platform ground monitoring system through the analogue instrument display mode.
The technical scheme that the utility model adopted is: a kind of unmanned vehicle physical simulation test platform ground monitoring system; Comprise: a machine three screen industrial control computers, the manual drive mechanism that links to each other with a machine three screen industrial control computers respectively, power supply, the data radio station and first to the 3rd display screen that communicate through data link and airborne test macro.
Also be provided with manual controller, described manual controller communicates through second data link and airborne test macro.
Described first display screen is the parameter display screen; Described second display screen is actual map track following figure display screen, and described the 3rd display screen is the display screen of relevant information that shows in real time performance parameter and the failure warning information and the steering order implementation status of unmanned vehicle physical model.
The performance parameter of described unmanned vehicle physical model comprises course angle, roll angle, the angle of pitch, speed and height.
The unmanned vehicle physical simulation test platform ground monitoring system of the utility model; Can in flight course, gather in real time the unmanned vehicle physical model parameters (comprise geographic coordinate information, attitude angle information, three shaft angle acceleration informations, course, highly, other information such as air speed) in; Offer the personnel of land station through the analogue instrument display mode; Make things convenient for the control of the personnel of land station through control command prompting frame and fault/warning message prompting frame, meanwhile carry out can also the expectation value of each item important parameter intuitively being contrasted in the actual acquisition value in the process in experiment to the unmanned vehicle physical model.The interface integrated level that comprises above function is high and succinct, and stable image data is in time continuous, helps physical simulation experiment, and the data automatic recording after test is accomplished has alleviated the personnel's of land station workload.The utility model has been realized the directly perceived and assessment reliably to the flight control system control algolithm.
Description of drawings
Fig. 1 is the one-piece construction block diagram of the utility model;
Fig. 2 is that airborne test macro constitutes block diagram.
Wherein:
1: one machine three screen industrial control computer 2: manual drive mechanism
3: data radio station 4: power supply
6: the second display screens of 5: the first display screens
Display screen 8 in 7: the three: airborne test macro
9: manual controller 10: data link
Data link 81 in 11: the second: the electrical source of power unit
82: sensor unit 83: central processor unit
84: analog switch 85: steering wheel group unit
86: airborne data radio station 87: remote-control receiver
89: the second receiving antennas of 88: the first receiving antennas
Embodiment
Below in conjunction with embodiment and accompanying drawing the unmanned vehicle physical simulation test platform ground monitoring system of the utility model is made detailed description.
As shown in Figure 1; The unmanned vehicle physical simulation test platform ground monitoring system of the utility model; Comprise: a machine three screen industrial control computers 1; The manual drive mechanism 2, power supply 4, data radio station 3 and first to the 3rd display screen 5,6,7 that link to each other with a machine three screen industrial control computers 1 respectively, described data radio station 3 communicates through data link 10 and airborne test macro 8.
The characteristic of the unmanned vehicle physical simulation test platform ground monitoring system of the utility model is in system, to have used a machine three screen industrial control computers to control the unmanned vehicle physical model and accomplishes self-navigation and attitude control; Wherein, Described first display screen 5 is the parameter display screen; Described second display screen 6 is actual map track following figure display screen; Described the 3rd display screen 7 is the display screen of relevant information that shows in real time performance parameter and failure warning information and the steering order implementation status of unmanned vehicle physical model, and the performance parameter of described unmanned vehicle physical model comprises course angle, roll angle, the angle of pitch, speed (air speed) and highly.
Also be provided with manual controller 9, described manual controller 9 communicates with airborne test macro 8 through second data link 11.(there are two separated links in ground monitoring system and airborne test macro communication; One for to carry out communication through data radio station; Ground monitoring system is installed data radio station 1; Airborne test macro is installed data radio station 2, and ground monitoring system carries out data transmission through this loop and airborne test macro under the proper testing running status, and automatic mode under the normal condition of ground and manual drive mechanism operating pattern be operation in the case all; Under the abnomal condition, when the data radio station data link breaks down, can pass through second wireless telecommunications individual event link, through the forced landing of control manual controller, this mode configuration is that airborne test macro is equipped with a hardware receiver in addition, and manual controller is built-in with transmitter.) when in testing the control rate flight test, mistake occurring, force to switch to the manual controller control model through software on ground, so that aircraft can safe landing or continuation execution aerial mission.
As shown in Figure 2; Described airborne test macro 8 includes sensor unit 82, central processor unit 83, analog switch 84 and the steering wheel group unit 85 that links to each other successively; Described central processor unit 83 also connects the airborne data radio station 86 that links to each other with first receiving antenna 88; Described analog switch 84 also connects the remote-control receiver 87 that links to each other with second receiving antenna 89; Remote-control receiver 87 one tunnel look-at-mes are connected to central processor unit 83, and remote-control receiver 87 other 4 road signals (throttle deviator, aileron rudder deviator, elevating rudder deviator, yaw rudder deviator) are connected to analog switch.Also be provided with the electrical source of power unit 81 that power supply is provided to each several part.
The unmanned vehicle physical simulation test platform ground monitoring system of the utility model; The parameter information that airborne test macro is collected the airborne sensor unit is handled the back through this internal system and is sent to ground monitoring system through airborne data radio station; Simultaneously airborne test macro also can respond the manual controller instruction and realize the control of aircraft physical model with the ground monitoring system steering order, the response priority can be when the aircraft physical model takes off by also switching controls pattern in real time in the ground setting flight course; Ground monitoring system one machine three screen industrial control computers receive the data that airborne test macro descends through data radio station; Through land station's software processes corresponding respectively output to the first to the 33 screen; Manual drive mechanism connects a machine three screen industrial control computers steering order is processed into the steering order that airborne equipment can be discerned through land station; The realization ground monitoring system is controlled automatically, and power supply provides the power supply of whole earth station system.
Claims (4)
1. unmanned vehicle physical simulation test platform ground monitoring system; It is characterized in that; Comprise: a machine three screen industrial control computers (1), the manual drive mechanism (2) that links to each other with a machine three screen industrial control computers (1) respectively, power supply (4), the data radio station (3) and first to the 3rd display screen (5,6,7) that communicate through data link (10) and airborne test macro (8).
2. unmanned vehicle physical simulation test platform ground monitoring system according to claim 1 is characterized in that, also is provided with manual controller (9), and described manual controller (9) communicates through second data link (11) and airborne test macro (8).
3. unmanned vehicle physical simulation test platform ground monitoring system according to claim 1; It is characterized in that; Described first display screen (5) is the parameter display screen; Described second display screen (6) is actual map track following figure display screen, and described the 3rd display screen (7) is the display screen of relevant information that shows in real time performance parameter and the failure warning information and the steering order implementation status of unmanned vehicle physical model.
4. unmanned vehicle physical simulation test platform ground monitoring system according to claim 3 is characterized in that, the performance parameter of described unmanned vehicle physical model comprises course angle, roll angle, the angle of pitch, speed and height.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN2011203890986U CN202533754U (en) | 2011-10-14 | 2011-10-14 | Ground monitoring system for unmanned vehicle physical simulated test platform |
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| Application Number | Priority Date | Filing Date | Title |
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| CN2011203890986U CN202533754U (en) | 2011-10-14 | 2011-10-14 | Ground monitoring system for unmanned vehicle physical simulated test platform |
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| CN202533754U true CN202533754U (en) | 2012-11-14 |
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| CN2011203890986U Expired - Fee Related CN202533754U (en) | 2011-10-14 | 2011-10-14 | Ground monitoring system for unmanned vehicle physical simulated test platform |
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Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103076748A (en) * | 2012-12-28 | 2013-05-01 | 哈尔滨工业大学 | Flight test system controlling machine with data monitoring function |
| CN103838152A (en) * | 2014-02-28 | 2014-06-04 | 北京航空航天大学 | Ground test device used for flight control system and control method |
| CN104503460A (en) * | 2014-12-05 | 2015-04-08 | 电子科技大学 | Ground station control system for universal unmanned aerial vehicle |
| CN104880961A (en) * | 2015-04-29 | 2015-09-02 | 北京理工大学 | Real-time simulation experiment system of multi-unmanned plane distributed synergetic hardware in loop |
| CN105068444A (en) * | 2015-07-28 | 2015-11-18 | 北京航空航天大学 | Universal unmanned aerial vehicle data link simulation system |
| CN105334753A (en) * | 2015-12-02 | 2016-02-17 | 上海航空电器有限公司 | Ground proximity warning visual simulation verification platform system and method |
| WO2016049924A1 (en) * | 2014-09-30 | 2016-04-07 | SZ DJI Technology Co., Ltd. | Systems and methods for flight simulation |
| CN106325103A (en) * | 2016-10-31 | 2017-01-11 | 安徽理工大学 | Semi-physical simulation test system of four-rotor unmanned aerial vehicle flight control system |
| WO2017219313A1 (en) * | 2016-06-23 | 2017-12-28 | SZ DJI Technology Co., Ltd. | Systems and methods for controlling movable object behavior |
| US10086954B2 (en) | 2014-10-27 | 2018-10-02 | SZ DJI Technology Co., Ltd. | UAV flight display |
| CN108646705A (en) * | 2018-04-16 | 2018-10-12 | 西安飞机工业（集团）有限责任公司 | A kind of airplane ground test interconnection of signals TT＆C system |
| US10134298B2 (en) | 2014-09-30 | 2018-11-20 | SZ DJI Technology Co., Ltd. | System and method for supporting simulated movement |
| CN109062078A (en) * | 2018-08-13 | 2018-12-21 | 中国科学院长春光学精密机械与物理研究所 | VTOL fixed-wing system for flight control computer simulation test platform |
| CN114577241A (en) * | 2022-03-02 | 2022-06-03 | 北京卫星环境工程研究所 | Optical fiber multi-module multi-parameter airborne independent test method |
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2011
- 2011-10-14 CN CN2011203890986U patent/CN202533754U/en not_active Expired - Fee Related
Cited By (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103076748A (en) * | 2012-12-28 | 2013-05-01 | 哈尔滨工业大学 | Flight test system controlling machine with data monitoring function |
| CN103838152B (en) * | 2014-02-28 | 2016-08-17 | 北京航空航天大学 | A kind of ground test device for flight control system and control method |
| CN103838152A (en) * | 2014-02-28 | 2014-06-04 | 北京航空航天大学 | Ground test device used for flight control system and control method |
| US10134299B2 (en) | 2014-09-30 | 2018-11-20 | SZ DJI Technology Co., Ltd | Systems and methods for flight simulation |
| US10134298B2 (en) | 2014-09-30 | 2018-11-20 | SZ DJI Technology Co., Ltd. | System and method for supporting simulated movement |
| WO2016049924A1 (en) * | 2014-09-30 | 2016-04-07 | SZ DJI Technology Co., Ltd. | Systems and methods for flight simulation |
| US11276325B2 (en) | 2014-09-30 | 2022-03-15 | SZ DJI Technology Co., Ltd. | Systems and methods for flight simulation |
| US9589476B2 (en) | 2014-09-30 | 2017-03-07 | SZ DJI Technology Co., Ltd | Systems and methods for flight simulation |
| CN106716272A (en) * | 2014-09-30 | 2017-05-24 | 深圳市大疆创新科技有限公司 | Systems and methods for flight simulation |
| US11217112B2 (en) | 2014-09-30 | 2022-01-04 | SZ DJI Technology Co., Ltd. | System and method for supporting simulated movement |
| US10086954B2 (en) | 2014-10-27 | 2018-10-02 | SZ DJI Technology Co., Ltd. | UAV flight display |
| CN104503460A (en) * | 2014-12-05 | 2015-04-08 | 电子科技大学 | Ground station control system for universal unmanned aerial vehicle |
| CN104880961A (en) * | 2015-04-29 | 2015-09-02 | 北京理工大学 | Real-time simulation experiment system of multi-unmanned plane distributed synergetic hardware in loop |
| CN105068444B (en) * | 2015-07-28 | 2017-08-25 | 北京航空航天大学 | A kind of universal Unmanned Aerial Vehicle Data Link analogue system |
| CN105068444A (en) * | 2015-07-28 | 2015-11-18 | 北京航空航天大学 | Universal unmanned aerial vehicle data link simulation system |
| CN105334753A (en) * | 2015-12-02 | 2016-02-17 | 上海航空电器有限公司 | Ground proximity warning visual simulation verification platform system and method |
| WO2017219313A1 (en) * | 2016-06-23 | 2017-12-28 | SZ DJI Technology Co., Ltd. | Systems and methods for controlling movable object behavior |
| CN106325103A (en) * | 2016-10-31 | 2017-01-11 | 安徽理工大学 | Semi-physical simulation test system of four-rotor unmanned aerial vehicle flight control system |
| CN108646705A (en) * | 2018-04-16 | 2018-10-12 | 西安飞机工业（集团）有限责任公司 | A kind of airplane ground test interconnection of signals TT＆C system |
| CN109062078A (en) * | 2018-08-13 | 2018-12-21 | 中国科学院长春光学精密机械与物理研究所 | VTOL fixed-wing system for flight control computer simulation test platform |
| CN114577241A (en) * | 2022-03-02 | 2022-06-03 | 北京卫星环境工程研究所 | Optical fiber multi-module multi-parameter airborne independent test method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20121114 Termination date: 20131014 |