CN205396577U - General unmanned aerial vehicle ground detection system - Google Patents
General unmanned aerial vehicle ground detection system Download PDFInfo
- Publication number
- CN205396577U CN205396577U CN201620133357.1U CN201620133357U CN205396577U CN 205396577 U CN205396577 U CN 205396577U CN 201620133357 U CN201620133357 U CN 201620133357U CN 205396577 U CN205396577 U CN 205396577U
- Authority
- CN
- China
- Prior art keywords
- industrial computer
- interface adapter
- detection system
- input
- outfan
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Abstract
The utility model provides a general unmanned aerial vehicle ground detection system, includes power input module, and power input module passes through power management module and is connected with interface adapter, PXI industrial computer, and the interface adapter input is connected with unmanned aerial vehicle flight control system, and interface adapter's output is connected with PXI industrial computer input through digital universal meter, multi -functional data collection card, multichannel relay, RS232, RS485 respectively, and the PXI industrial computer is connected with keyboard module and display module, the utility model discloses can carry out comprehensive comprehensive testing to complicated unmanned aerial vehicle flight control system to can changing corresponding interface adapter and changing the relevant parameter setting according to different models, make the unmanned aerial vehicle ground detection system have the commonality, small, intelligent degree is high, can effectively get rid of the trouble hidden danger of unmanned aerial vehicle equipment, ensures the reliable efficient of aircraft mission and accomplishes.
Description
Technical field
This utility model relates to unmanned plane detection technique field, particularly relates to a kind of general unmanned machine ground detection system.
Background technology
Unmanned plane has the man-machine flight limit that cannot complete owing to can reach, and has again information real-time and controllability, it is possible to achieve the superior ratio of performance to price compared with satellite.Along with the development of aviation and electronic technology, novel unmanned plane during flying performance is increasingly stronger, and task device is also more and more superior.But, due to unpiloted reason, the potential faults of airborne equipment and in-flight produced problem are difficult to obtain process proper in time as manned aircraft, and therefore the accident rate of unmanned plane is man-machine apparently higher than having.And the detection of existing unmanned aerial vehicle system control equipment is single, complex operation, versatility are poor.
Summary of the invention
For the shortcoming overcoming above-mentioned prior art, the purpose of this utility model is in that to provide a kind of general unmanned machine ground detection system, enhance the versatility of unmanned plane detection control equipment, detect before unmanned plane can be taken off and daily preservation & testing, particularly before take-off the critical component on machine and visual plant are carried out on-line checking or analog manipulation, to confirm whole unmanned plane duty, it is ensured that aerial mission satisfactorily effectively completes.
In order to achieve the above object, the technical scheme that this utility model is taked is:
nullA kind of general unmanned machine ground detection system，Including Power Entry Module 2，The outfan of Power Entry Module 2 is connected with the input of power management module 3，First outfan of power management module 3 is connected with the first input end of interface adapter 1，Second input/output terminal of power management module 3 and PXI industrial computer 9 are bi-directionally connected，Second input of interface adapter 1 is connected with the outfan of system for flight control computer 12，First outfan of interface adapter 1 is connected with the first input end of PXI industrial computer 9 by digital multimeter 4，Second outfan of interface adapter 1 is connected with the second input of PXI industrial computer 9 by multifunctional data acquisition card 5，3rd outfan of interface adapter 1 is connected with the 3rd input of PXI industrial computer 9 by multichannel relay 6，4th outfan of interface adapter 1 is connected by the four-input terminal of RS2327 and PXI industrial computer 9，5th outfan of interface adapter 1 is connected by the 5th input of RS4858 and PXI industrial computer 9，6th input of PXI industrial computer 9 is connected with the outfan of Keysheet module 11，The outfan of PXI industrial computer 9 is connected with display module 10.
Described interface adapter 1 is the passage that PXI industrial computer 9 is connected with system for flight control computer 12.
Described Power Entry Module 2 output single-phase power frequency 220V alternating current power supply.
Described power management module 3 detects system power supply by input voltage carries out conversion output 28V unmanned plane multiple power source and 15V.
Described digital multimeter 4 completes the measurement to unmanned plane motor cylinder temperature resistance.
System for flight control computer 12 signal is acquired by described multifunctional data acquisition card 5.
The various signals that turnover flies to control are carried out the selection of signal source by described multichannel relay 6.
Described PXI industrial computer 9 is for on-off state, voltage, electric current, the collection of temperature simulation amount, detection and control.
Power supply, electromechanics, fuel system state, on-off state and testing result are displayed by described display module 10.
Described Keysheet module 11 is correspondingly arranged different avionics parameters according to different unmanned plane types, thus unmanned plane is detected.
The utility model has the advantage of: complicated system for flight control computer can be carried out Comprehensive detection, and can according to different type of machines, change corresponding interface adapter and change relative parameters setting, unmanned aerial vehicle detection system is made to have versatility, volume is little, intelligence degree is high, it is possible to effectively get rid of the potential faults of unmanned plane equipment, it is ensured that aerial mission is reliably efficiently completed.
Accompanying drawing explanation
Accompanying drawing is structured flowchart of the present utility model.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model is described in further detail.
nullWith reference to accompanying drawing，A kind of general unmanned machine ground detection system，Including Power Entry Module 2，The outfan of Power Entry Module 2 is connected with the input of power management module 3，First outfan of power management module 3 is connected with the first input end of interface adapter 1，Second input/output terminal of power management module 3 and PXI industrial computer 9 are bi-directionally connected，Second input of interface adapter 1 is connected with the outfan of system for flight control computer 12，First outfan of interface adapter 1 is connected with the first input end of PXI industrial computer 9 by digital multimeter 4，Second outfan of interface adapter 1 is connected with the second input of PXI industrial computer 9 by multifunctional data acquisition card 5，3rd outfan of interface adapter 1 is connected with the 3rd input of PXI industrial computer 9 by multichannel relay 6，4th outfan of interface adapter 1 is connected by the four-input terminal of RS2327 and PXI industrial computer 9，5th outfan of interface adapter 1 is connected by the 5th input of RS4858 and PXI industrial computer 9，6th input of PXI industrial computer 9 is connected with the outfan of Keysheet module 11，The outfan of PXI industrial computer 9 is connected with display module 10.
Described interface adapter 1 is the passage that PXI industrial computer 9 is connected with system for flight control computer 12.
Described Power Entry Module 2 output single-phase power frequency 220V alternating current power supply.
Described power management module 3 detects system power supply by input voltage carries out conversion output 28V unmanned plane multiple power source and 15V.
Described digital multimeter 4 completes the measurement to unmanned plane motor cylinder temperature resistance.
System for flight control computer 12 signal is acquired by described multifunctional data acquisition card 5.
The various signals that turnover flies to control are carried out the selection of signal source by described multichannel relay 6.
Described RS2327 realize ground detection system with fly control 232 serial ports and course transmitter carry out communication.
Described RS4858 realize ground detection system with fly control 422 serial ports and inertial navigation carry out communication.
Described PXI industrial computer 9 is for on-off state, voltage, electric current, the collection of temperature simulation amount, detection and control.
Power supply, electromechanics, fuel system state, on-off state and testing result are displayed by described display module 10.
Described Keysheet module 11 is correspondingly arranged different avionics parameters according to different unmanned plane types, thus unmanned plane is detected.
Operation principle of the present utility model is: PXI industrial computer 9 is connected with system for flight control computer 12 by interface adapter 1, PXI industrial computer 9 detects flying control output signal, by carrying out processing to signal collected and assess, complete the detection of duty to airborne equipments such as unmanned plane course transmitter, inertial navigation, electromotor, steering wheels, and testing result is displayed by display module 10, the pre-flight state knowing unmanned plane that can be simple and clear according to testing result.By changing matching interface adapter 1 and revising relevant parameter design by Keysheet module 11, it is possible to the unmanned plane of different type of machines is detected.
Claims (10)
- null1. a general unmanned machine ground detection system，Including Power Entry Module (2)，The outfan of Power Entry Module (2) is connected with the input of power management module (3)，First outfan of power management module (3) is connected with the first input end of interface adapter (1)，Second input/output terminal of power management module (3) and PXI industrial computer (9) are bi-directionally connected，It is characterized in that: the second input of interface adapter (1) is connected with the outfan of system for flight control computer (12)，First outfan of interface adapter (1) is connected with the first input end of PXI industrial computer (9) by digital multimeter (4)，Second outfan of interface adapter (1) is connected with the second input of PXI industrial computer (9) by multifunctional data acquisition card (5)，3rd outfan of interface adapter (1) is connected with the 3rd input of PXI industrial computer (9) by multichannel relay (6)，4th outfan of interface adapter (1) is connected with the four-input terminal of PXI industrial computer (9) by RS232 (7)，5th outfan of interface adapter (1) is connected with the 5th input of PXI industrial computer (9) by RS485 (8)，6th input of PXI industrial computer (9) is connected with the outfan of Keysheet module (11)，The outfan of PXI industrial computer (9) is connected with display module (10).
- 2. the general unmanned machine ground detection system of one according to claim 1, it is characterised in that: described interface adapter (1) is the passage that PXI industrial computer (9) is connected with system for flight control computer (12).
- 3. the general unmanned machine ground detection system of one according to claim 1, it is characterised in that: described Power Entry Module (2) output single-phase power frequency 220V alternating current power supply.
- 4. the general unmanned machine ground detection system of one according to claim 1, it is characterised in that: described power management module (3) detects system power supply by input voltage carries out conversion output 28V unmanned plane multiple power source and 15V.
- 5. the general unmanned machine ground detection system of one according to claim 1, it is characterised in that: described digital multimeter (4) completes the measurement to unmanned plane motor cylinder temperature resistance.
- 6. the general unmanned machine ground detection system of one according to claim 1, it is characterised in that: system for flight control computer (12) signal is acquired by described multifunctional data acquisition card (5).
- 7. the general unmanned machine ground detection system of one according to claim 1, it is characterised in that: the various signals that turnover flies to control are carried out the selection of signal source by described multichannel relay (6).
- 8. the general unmanned machine ground detection system of one according to claim 1, it is characterised in that: described PXI industrial computer (9) is for on-off state, voltage, electric current, the collection of temperature simulation amount, detection and control.
- 9. the general unmanned machine ground detection system of one according to claim 1, it is characterised in that: power supply, electromechanics, fuel system state, on-off state and testing result are displayed by described display module (10).
- 10. the general unmanned machine ground detection system of one according to claim 1, it is characterised in that: described Keysheet module (11) is correspondingly arranged different avionics parameters according to different unmanned plane types, thus unmanned plane is detected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620133357.1U CN205396577U (en) | 2016-02-22 | 2016-02-22 | General unmanned aerial vehicle ground detection system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620133357.1U CN205396577U (en) | 2016-02-22 | 2016-02-22 | General unmanned aerial vehicle ground detection system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205396577U true CN205396577U (en) | 2016-07-27 |
Family
ID=56445385
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620133357.1U Expired - Fee Related CN205396577U (en) | 2016-02-22 | 2016-02-22 | General unmanned aerial vehicle ground detection system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205396577U (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106197474A (en) * | 2016-08-26 | 2016-12-07 | 云南电网有限责任公司 | A kind of high altitude localities helicopter flight condition checkout gear |
| CN106586028A (en) * | 2016-12-23 | 2017-04-26 | 北京安达维尔科技股份有限公司 | System for testing aviation part |
| CN106780831A (en) * | 2016-11-24 | 2017-05-31 | 陕西千山航空电子有限责任公司 | It is a kind of can online programming general winged ginseng collector |
| CN106919184A (en) * | 2016-12-20 | 2017-07-04 | 北京理工大学 | Double unmanned plane coordinated operation systems and double unmanned plane work compound methods |
| CN106980057A (en) * | 2017-03-30 | 2017-07-25 | 华映科技（集团）股份有限公司 | A kind of unmanned plane based on intelligent and safe electricity system perceives method for early warning |
| CN109030050A (en) * | 2018-07-25 | 2018-12-18 | 成都飞机工业（集团）有限责任公司 | Testing device of steering engine and its test method on a kind of machine |
| CN109211602A (en) * | 2018-07-25 | 2019-01-15 | 成都飞机工业（集团）有限责任公司 | Testing device of steering engine and its test method on a kind of machine |
| 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 |
| CN114721358A (en) * | 2022-05-10 | 2022-07-08 | 中国民航大学 | Technology for testing ground function of flight control system and switching device |
-
2016
- 2016-02-22 CN CN201620133357.1U patent/CN205396577U/en not_active Expired - Fee Related
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106197474A (en) * | 2016-08-26 | 2016-12-07 | 云南电网有限责任公司 | A kind of high altitude localities helicopter flight condition checkout gear |
| CN106780831A (en) * | 2016-11-24 | 2017-05-31 | 陕西千山航空电子有限责任公司 | It is a kind of can online programming general winged ginseng collector |
| CN106919184A (en) * | 2016-12-20 | 2017-07-04 | 北京理工大学 | Double unmanned plane coordinated operation systems and double unmanned plane work compound methods |
| CN106919184B (en) * | 2016-12-20 | 2019-12-13 | 北京理工大学 | Double-unmanned-aerial-vehicle cooperative operation system and double-unmanned-aerial-vehicle cooperative operation method |
| CN106586028A (en) * | 2016-12-23 | 2017-04-26 | 北京安达维尔科技股份有限公司 | System for testing aviation part |
| CN106980057A (en) * | 2017-03-30 | 2017-07-25 | 华映科技（集团）股份有限公司 | A kind of unmanned plane based on intelligent and safe electricity system perceives method for early warning |
| CN106980057B (en) * | 2017-03-30 | 2019-08-16 | 华映科技（集团）股份有限公司 | A kind of intelligent and safe electricity system |
| CN109030050A (en) * | 2018-07-25 | 2018-12-18 | 成都飞机工业（集团）有限责任公司 | Testing device of steering engine and its test method on a kind of machine |
| CN109211602A (en) * | 2018-07-25 | 2019-01-15 | 成都飞机工业（集团）有限责任公司 | Testing device of steering engine and its test method on a kind of machine |
| 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 |
| CN114721358A (en) * | 2022-05-10 | 2022-07-08 | 中国民航大学 | Technology for testing ground function of flight control system and switching device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205396577U (en) | General unmanned aerial vehicle ground detection system | |
| CN202093395U (en) | Earth station remote control device for unmanned vehicle | |
| CN203950036U (en) | A kind of have people's depopulated helicopter anti-collision system based on millimetre-wave radar range finding | |
| CN203551961U (en) | Avionics hardware-in-the-loop simulation system for unmanned plane | |
| CN205540284U (en) | A joint control system for unmanned aerial vehicle | |
| CN202694152U (en) | Unmanned aerial vehicle control system | |
| CN104808675A (en) | Intelligent terminal-based somatosensory flight operation and control system and terminal equipment | |
| CN202632111U (en) | Electric field measurement obstacle avoidance system for polling live wire by unmanned aerial vehicle | |
| CN102722178A (en) | Electric field measuring obstacle avoidance system and method for live wire routing inspection of unmanned aerial vehicle | |
| CN103925853B (en) | A kind of carrier rocket ground testing system device | |
| CN104503460A (en) | Ground station control system for universal unmanned aerial vehicle | |
| CN105334861A (en) | Unmanned plane flight control module, unmanned plane flight control system and unmanned plane | |
| CN102736632A (en) | Differential evadible system of electric field for unmanned aerial vehicle polling live wires and method | |
| CN109709986A (en) | A kind of unmanned aerial vehicle control system and method | |
| CN202632112U (en) | Electric field difference obstacle avoidance system for live wire tour inspection of unmanned aerial vehicle | |
| CN110501667B (en) | Test system and ground test method of ultrashort wave orientation instrument | |
| CN106855693A (en) | A kind of near space aerostatics semi-physical system, avionics system test and winged control semi-physical simulation method and ground controlling method | |
| CN105676873A (en) | Automatic landing method and control system of unmanned aerial vehicle | |
| CN105067898B (en) | A kind of device for lighting location | |
| RU162771U1 (en) | UNMANNED AEROMAGNETIC COMPLEX (BAMK) | |
| CN204856926U (en) | Multi -functional data conversion system based on airborne collision avoidance system | |
| CN206906894U (en) | A kind of UAV Flight Control management system | |
| CN109143166B (en) | Ultra-long-distance unmanned aerial vehicle navigation method | |
| CN205265802U (en) | Unmanned aerial vehicle machine carries controlling means of camera | |
| CN106125638A (en) | A kind of airborne teledata concentrator based on bus output |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160727 Termination date: 20190222 |