CN202617351U - Wireless positioning and monitoring system for ultra-light flight vehicle - Google Patents
Wireless positioning and monitoring system for ultra-light flight vehicle Download PDFInfo
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- CN202617351U CN202617351U CN 201220156879 CN201220156879U CN202617351U CN 202617351 U CN202617351 U CN 202617351U CN 201220156879 CN201220156879 CN 201220156879 CN 201220156879 U CN201220156879 U CN 201220156879U CN 202617351 U CN202617351 U CN 202617351U
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- interface circuit
- microlight
- control system
- base plate
- wireless location
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Abstract
The utility model relates to a monitoring system, and particularly provides a wireless positioning and monitoring system for an ultra-light flight vehicle which is composed of a vehicle-mounted terminal and a monitoring center, wherein the vehicle-mounted terminal and the monitoring center exchange information through a communication link. Compared with the prior art, the wireless positioning and monitoring system provided by the utility model has the characteristics of light weight, small size, simple and compact structure, convenient operation, high reliability, and high data transmission speed.
Description
Technical field
The utility model relates to a kind of supervisory control system, specifically provides a kind of microlight-type aircraft and uses the wireless location supervisory control system.
Background technology
China will open gradually the spatial domain below 1000 meters, allow some baby plane flights such as light fixed-wing aircraft and helicopter.Because country relaxes the civil aircraft policy, civilian ultra-light aircraft will obtain increasing application.Supervision to the microlight-type aircraft also is that thing must gone so, comprises information such as airborne vehicle state of flight, flight path, job area, all will monitor the back-up storage with information in real time, so that later stage inquiry and supervision.
Summary of the invention
The utility model is to above problem; Provide a kind of microlight-type aircraft to use the wireless location supervisory control system; It utilizes new and high technologies such as global positioning system (GPS), GIS-Geographic Information System (GIS), 3G communication network; Send to the Surveillance center on ground to the real time position of airborne vehicle and state information through wireless network, the state of airborne vehicle is carried out real-time tracking and monitoring by Surveillance center.Native system has been realized functions such as the accurate location, route tracking, voice call, the warning of ultra spatial domain to aircraft.
The utility model solves the technical scheme that its technical problem adopted:
A kind of microlight-type aircraft is used the wireless location supervisory control system, is made up of Airborne Terminal and Surveillance center, realizes information interaction through communication link between Airborne Terminal and the Surveillance center.
Airborne Terminal is made up of main control module and base plate, and said main control module is connected power circuit respectively with base plate, links to each other through the USB mouth between said main control module and the base plate.
Base plate is made up of 3G module interface circuit, SIM interface circuit, indicator light interface circuit and voice call interface circuit, and described 3G module interface circuit, SIM interface circuit, indicator light interface circuit and voice call interface circuit are connected the central processing unit of main control module respectively through the USB mouth.
A kind of microlight-type aircraft of the utility model is used the wireless location supervisory control system; Airborne Terminal: the satellite positioning functions of mainly realizing airborne vehicle; To receive gps data (longitude and latitude, highly, time, speed etc.) and resolve, to data handle and pack after be uploaded to the data server of Surveillance center more in real time through 3G network.
Communication link: accomplish the bidirectional data transfers and the voice call of Airborne Terminal and Surveillance center.
Surveillance center: accomplish functions such as storage, Remote and wireless air upgrading to airborne portable terminal.Monitoring central server is resolved the packet of receiving, and in conjunction with generalized information system, can on electronic chart, show the positional information of current airborne vehicle clearly, and log and the state information with airborne vehicle stores several storehouses into simultaneously, supplies monitor staff's monitoring and inquiry.
Airborne Terminal has the data parsing ability, judges the state of airborne vehicle voluntarily, sends alarm signal when flying in the ultra spatial domain of airborne vehicle, and the ground monitoring center is issued with warning message simultaneously in prompting pilot overshoot flight field; The pilot also can carry out voice call through the Surveillance center on airborne mobile terminal calling ground.
The beneficial effect of the utility model is: 1) each intermodule adopts the usb bus mode to communicate by letter, and the output transmission speed is fast.2) CPU that adopts the ARM9 framework is as central processing unit, and the speed of service is fast, and data-handling capacity is strong.3) adopting embedded OS is software platform, and system's operation stability is high.4) pilot can carry out voice call through terminal and Surveillance center.5) terminal has data-handling capacity, judges the state of aircraft voluntarily, and alarm 6 when exceeding flight range) terminal and Surveillance center carry out data communication based on 3G network, and data transmission bauds is fast, but data amount transmitted is big.7) user can be connected to the server of Surveillance center through the mode of webpage, inquires about the details of aircraft, real-time flight path and flight historical record.8) system parameters of terminal equipment can be made amendment through monitoring software.
Compared with prior art, a kind of microlight-type aircraft of the utility model is used the wireless location supervisory control system, its have in light weight, volume is little, simple and compact for structure, easy to operate, reliability is high, data transmission bauds is fast characteristics.
Description of drawings
Fig. 1 is the overall structure sketch map of a kind of microlight-type aircraft with the wireless location supervisory control system;
Fig. 2 is the structured flowchart of a kind of microlight-type aircraft with the Airborne Terminal of wireless location supervisory control system;
Fig. 3 is the circuit theory diagrams of a kind of microlight-type aircraft with the 3G module interface circuit of the Airborne Terminal of wireless location supervisory control system;
Fig. 4 is the circuit theory diagrams of a kind of microlight-type aircraft with the SIM interface circuit of the Airborne Terminal of wireless location supervisory control system;
Fig. 5 is the circuit theory diagrams of a kind of microlight-type aircraft with the indicator light interface circuit of the Airborne Terminal of wireless location supervisory control system;
Fig. 6 is the circuit theory diagrams of a kind of microlight-type aircraft with the power circuit of the Airborne Terminal of wireless location supervisory control system.
Embodiment
Below in conjunction with accompanying drawing and specific embodiment a kind of microlight-type aircraft of the utility model is done further to describe with the wireless location supervisory control system.
Shown in accompanying drawing 1, a kind of microlight-type aircraft is used the wireless location supervisory control system, is made up of with Surveillance center 2 Airborne Terminal 1, realizes information interaction through communication link 3 between Airborne Terminal 1 and the Surveillance center 2.
Shown in accompanying drawing 2, Airborne Terminal 1 is made up of main control module 11 and base plate 12, and said main control module 11 is connected power circuit 13 respectively with base plate 12, links to each other through USB mouth 14 between said main control module 11 and the base plate 12.
Above-described embodiment, the utility model embodiment a kind of more preferably just, common variation that those skilled in the art carries out in the utility model technical scheme scope and replacement all should be included in the protection range of the utility model.
Claims (3)
1. a microlight-type aircraft is used the wireless location supervisory control system, is made up of Airborne Terminal and Surveillance center, it is characterized in that, realizes information interaction through communication link between said Airborne Terminal and the Surveillance center.
2. a kind of microlight-type aircraft according to claim 1 is used the wireless location supervisory control system; It is characterized in that; Described Airborne Terminal is made up of main control module and base plate, and said main control module is connected power circuit respectively with base plate, links to each other through the USB mouth between said main control module and the base plate.
3. a kind of microlight-type aircraft according to claim 2 is used the wireless location supervisory control system; It is characterized in that; Described base plate is made up of 3G module interface circuit, SIM interface circuit, indicator light interface circuit and voice call interface circuit, and described 3G module interface circuit, SIM interface circuit, indicator light interface circuit and voice call interface circuit are connected the central processing unit of main control module respectively through the USB mouth.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220156879 CN202617351U (en) | 2012-04-13 | 2012-04-13 | Wireless positioning and monitoring system for ultra-light flight vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220156879 CN202617351U (en) | 2012-04-13 | 2012-04-13 | Wireless positioning and monitoring system for ultra-light flight vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202617351U true CN202617351U (en) | 2012-12-19 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220156879 Expired - Fee Related CN202617351U (en) | 2012-04-13 | 2012-04-13 | Wireless positioning and monitoring system for ultra-light flight vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202617351U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106803385A (en) * | 2017-04-09 | 2017-06-06 | 中国人民解放军空军航空大学飞行研究所 | Assessment system is examined in a kind of flight supplemental training |
-
2012
- 2012-04-13 CN CN 201220156879 patent/CN202617351U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106803385A (en) * | 2017-04-09 | 2017-06-06 | 中国人民解放军空军航空大学飞行研究所 | Assessment system is examined in a kind of flight supplemental training |
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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 |
Granted publication date: 20121219 Termination date: 20180413 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |