CN203217082U - Remotely-controlled flight GPS geographic information collection system - Google Patents
Remotely-controlled flight GPS geographic information collection system Download PDFInfo
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- CN203217082U CN203217082U CN 201320228082 CN201320228082U CN203217082U CN 203217082 U CN203217082 U CN 203217082U CN 201320228082 CN201320228082 CN 201320228082 CN 201320228082 U CN201320228082 U CN 201320228082U CN 203217082 U CN203217082 U CN 203217082U
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Abstract
The utility model discloses a remotely-controlled flight GPS geographic information collection system and particularly, relates to a system that enables a GPS receiver, a range finder, a camera, and an on-board controller and the like to be installed at an aircraft and uses a ground control system to carry out operations on the components to realize GPS geographic information collection. At present, when longitude, latitude and altitude information of a designated place is collected, time and effort are wasted, the efficiency is low, and the personal safety is even threatened; however, with utilization of the system, the technical problems can be solved. The provided system is composed of an air vehicle and a ground controller for controlling the air vehicle; an on-board controller, a GPS receiver, a range finder, a camera, and an indicator are carried at the air vehicle, wherein the GPS receiver, the range finder, the camera, and the indicator are connected with the on-board controller; and the on-board controller and the ground controller are in communication connection. According to the system, with utilization of the structure, the working environment is safe; the system can be operated simply and conveniently; the work efficiency is high; and the whole time-saving, worry-free, and labor-saving measuring process is realized.
Description
Technical field
The utility model relates to a kind of remote control distributor GPS geographical information collection system, be specifically related to a kind of GPS receiver, stadimeter, video camera, indicator, on-board controller etc. are installed on the aircraft, by ground control system its operation realized the system that the GPS geographic information data is gathered.
Background technology
Survey, often need to gather in the field operation activity such as geologic prospecting longitude and latitude and the altitude information of appointed place on ground mapping, the boundary of a piece of land.Present normally used survey instrument is a kind of surveying instrument that the GPS main frame is installed at the holding rod top, by manually grasping this instrument to place to be measured, with the thin testing data that waits equipment and GPS main-machine communication and the current place of reading and recording of hand.But, much measure the place in the inaccessible places of people such as high mountain, danger slope, steep cliff, cliffs, when being measured, such place wastes time and energy, inefficiency, in the time of seriously even the entail dangers to personal safety.
The utility model content
The technical problems to be solved in the utility model be waste time and energy when surveying, gathering in the field operation activity such as geologic prospecting the longitude and latitude of appointed place and altitude information on ground mapping, the boundary of a piece of land, inefficiency, even the entail dangers to personal safety, a kind of remote control distributor GPS geographical information collection system with low cost, simple to operate, easy to use is provided.
For achieving the above object, the utility model adopts following technical proposals: a kind of remote control distributor GPS geographical information collection system, it comprises the ground controller of aircraft and control aircraft, the on-board controller that carries at described aircraft and GPS receiver, stadimeter, video camera, the indicator that is connected with on-board controller, described on-board controller is connected with the ground controller communication.
Described aircraft is four rotor crafts, comprises aircraft fuselage, is positioned at the screw propeller of aircraft fuselage periphery and places the rotor of screw propeller top.
Totally four on described screw propeller is the decussation structure.
Described on-board controller comprises the master control chip
, the master control chip
Input end connect GPS receiver, stadimeter, video camera, indicator, its output terminal connects wireless data transfer module
With the wireless video sending module
Described stadimeter is laser range finder or ultrasonic range finder or altitude gauge.
Described indicator is laser designator.
Described ground controller comprises the master control chip
, the master control chip
Be connected with wireless data transfer module
, the wireless video receiver module
, monitor, guidance panel and storer, wherein monitor places the top of guidance panel.
Adopt the utility model of technique scheme, when surveying, needing in the field operation activity such as geologic prospecting to gather the longitude and latitude of appointed place and altitude information on ground mapping, the boundary of a piece of land, only need the operate ground controller just can finish the measurement of certain measurement point, working environment is safer, simple and convenient, work efficiency is higher, and whole measuring process saves time, saves worry, laborsaving.
Description of drawings
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the formation diagram of on-board controller.
Fig. 3 is the structural representation of ground controller.
Fig. 4 is the formation diagram of ground controller.
Fig. 5 is aircraft measurement system control flow chart.
Fig. 6 is the ground controller control flow chart.
Embodiment
As shown in Figure 1, the utility model comprises the ground controller 7 of aircraft 1 and control aircraft 1, the on-board controller 6 that carries at described aircraft 1 and the GPS receiver 2 that is connected with on-board controller 6, stadimeter 3, video camera 4, indicator 5, described on-board controller 6 is connected with ground controller 7 communications.
Described aircraft 1 is four rotor crafts, comprises aircraft fuselage 11, is positioned at the screw propeller 12 of aircraft fuselage 11 peripheries and places the rotor 13 of screw propeller 12 tops; Totally four on screw propeller 12 is the decussation structure.This kind aircraft can be under multiple environmental baseline vertical takeoff and landing, under the effect of flight control system, can hover with multiple attitude flight, precedingly fly, side flies and inverted flight.Usually video camera 4 and the wireless video sending module that loads on the aircraft is sent to ground controller 7 with real-time video and is presented on the monitor 72, can assign the flight steering order and adjusts flight attitude by observing monitor 72.
Described GPS receiver adopts the metering system of differential GPS usually, namely by in that fixedly survey station and mobile survey station carry out simultaneous observation, send correction by base station, by the satnav of positioning result on subscriber station reception and the mobile survey station of correction, to obtain the accurate localization result.For obtaining the measurement result of accurate altitude information, load stadimeter on the aircraft usually, the altitude information that GPS is recorded deducts the flying height that stadimeter or altitude gauge record, and obtains topocentric altitude information to be measured.
Described on-board controller 6 comprises the master control chip
, the master control chip
Input end connect GPS receiver 2, stadimeter 3, video camera 4, indicator 5, its output terminal connects wireless data transfer module
With the wireless video sending module
As shown in Figure 2, the master control chip receives the flight steering order that ground controller 7 is sent by wireless data transfer module, by flight control system, and regulation and control flying speed and attitude, and a data that record sends to ground controller.Usually the master control chip also is responsible for configuration and unlatching, the configuration of GPS receiver and the unlatching of unlatching and laser designator of wireless video sending module.
Described stadimeter 3 is laser range finder or ultrasonic range finder or altitude gauge.
Described indicator 5 is laser designator.
Described ground controller 7 comprises the master control chip
, the master control chip
Be connected with wireless data transfer module
, the wireless video receiver module
, monitor 72, guidance panel 71 and storer 73,, wherein monitor 72 places the top of guidance panel 71.Ground controller comprises the master control chip
, the master control chip
Be connected with wireless data transfer module
, the wireless video receiver module
, monitor, guidance panel and storer.As shown in Figure 3, its effect is that user instruction is sent to aircraft, control aircraft flight attitude, and receive the storage gps measurement data, the monitor effect is that the video that the monitoring aircraft transmits is in real time adjusted flight attitude to make things convenient for the user, seeks measurement point; Internal circuit mainly comprises storer, master control chip, wireless data transfer module, wireless video receiver module, as shown in Figure 4, the user passes through guidance panel, instruction is sent to the master control chip, the master control chip will instruct coding and send to aircraft by wireless data transfer module, receive the data that GPS records and will store by the wireless data transmission.Usually comprise the wireless video receiver module, the real time video signals that the wireless video sending module that is used for loading on the reception aircraft is sent.
Below in conjunction with accompanying drawing, the utility model is done specific descriptions:
Need before the use earlier equipment to be carried out integral body inspection, comprise in the scope of examination: the electric power thus supplied of watching aircraft 1 and ground controller 7, the mechanical part of check flight device 1 has or not insufficient lubrication etc. unusual, whether the situation that checks each airborne equipment is normal ... if all are normal, assign the instruction of taking off.
Operate ground controller 7, remotely-piloted vehicle 1 flight is to top, place to be measured.Can send the flight steering order by observation flight device position and attitude in the remote control process, also can send instruction and open airborne video camera 4, real-time video is sent to ground controller 7 and in monitor 72 demonstrations, sends the flight steering order by checking monitor 72.
When aircraft 1 arrives top to be measured, if airborne video camera 4 is not opened, then with its unlatching, real-time video is sent to ground controller 7 and in monitor 72 demonstrations.Open laser designator 5, the indication laser beam is observed monitor 72 with vertical directive ground, when the laser spots on directive ground during over against measurement point, assigns and measures instruction.
Aircraft 1 is received and is measured instruction, the locking measurement point, treat that aircraft is stable after, read gps measurement data.If laser range finder 3 is opened, then read the flying height that laser range finder 3 records, and the data that record are sent to ground controller 7, finish the measurement of a measurement point.
Continue if desired to measure, then remotely-piloted vehicle 1 flies to next measurement point, repeats above-mentioned steps and measures.If test is finished, then make a return voyage.
Can be used in needs such as the boundary of a piece of land surveys, ground mapping in the utility model and measure the occasion of formulating place gps coordinate information.
Claims (7)
1. remote control distributor GPS geographical information collection system, comprise the GPS measuring instrument, it is characterized in that: it comprises the ground controller (7) of aircraft (1) and control aircraft (1), be equipped with on-board controller (6) and the GPS receiver (2) that is connected with on-board controller (6), stadimeter (3), video camera (4), indicator (5) at described aircraft (1), described on-board controller (6) is connected with ground controller (7) communication.
2. remote control distributor GPS geographical information collection according to claim 1 system, it is characterized in that: described aircraft (1) is four rotor crafts, comprises aircraft fuselage (11), is positioned at the screw propeller (12) of aircraft fuselage (11) periphery and places rotor (13) above the screw propeller (12).
3. remote control distributor GPS geographical information collection according to claim 2 system, it is characterized in that: totally four on described screw propeller (12) is the decussation structure.
4. remote control distributor GPS geographical information collection according to claim 1 system, it is characterized in that: described on-board controller (6) comprises the master control chip
, the master control chip
Input end connect GPS receiver (2), stadimeter (3), video camera (4), indicator (5), its output terminal connects wireless data transfer module
With the wireless video sending module
5. according to claim 1 or 4 described remote control distributor GPS geographical information collection systems, it is characterized in that: described stadimeter (3) is laser range finder or ultrasonic range finder or altitude gauge.
6. according to claim 1 or 4 described remote control distributor GPS geographical information collection systems, it is characterized in that: described indicator (5) is laser designator.
7. remote control distributor GPS geographical information collection according to claim 1 system, it is characterized in that: described ground controller (7) comprises the master control chip
, the master control chip
Be connected with wireless data transfer module
, the wireless video receiver module
, monitor (72), guidance panel (71) and storer (73), wherein monitor (72) places the top of guidance panel (71).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320228082 CN203217082U (en) | 2013-04-28 | 2013-04-28 | Remotely-controlled flight GPS geographic information collection system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320228082 CN203217082U (en) | 2013-04-28 | 2013-04-28 | Remotely-controlled flight GPS geographic information collection system |
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| Publication Number | Publication Date |
|---|---|
| CN203217082U true CN203217082U (en) | 2013-09-25 |
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| CN 201320228082 Expired - Fee Related CN203217082U (en) | 2013-04-28 | 2013-04-28 | Remotely-controlled flight GPS geographic information collection system |
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Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103699133A (en) * | 2013-12-12 | 2014-04-02 | 西安交通大学 | Multi-aircraft hoisting coordinated control system |
| CN104267741A (en) * | 2014-09-12 | 2015-01-07 | 深圳市创新智慧港有限公司 | Aerial photography device with intelligent steering function |
| CN104519314A (en) * | 2013-12-25 | 2015-04-15 | 柳州桂通科技有限公司 | Quick acquisition method of panoramic information of accident site |
| CN104519315A (en) * | 2013-12-25 | 2015-04-15 | 柳州桂通科技有限公司 | Accident scene panoramic information fast collecting device |
| CN105159318A (en) * | 2015-09-23 | 2015-12-16 | 郑州大学 | Ecological civilization monitoring device and system |
| CN105204516A (en) * | 2015-09-23 | 2015-12-30 | 郑州大学 | Biological agriculture monitoring method, device and system |
| CN105242682A (en) * | 2015-11-04 | 2016-01-13 | 北京航天科颐技术有限公司 | Target characteristic measurement system for drone aircraft |
| CN105262986A (en) * | 2015-09-23 | 2016-01-20 | 郑州大学 | Equipment and system for tracing and monitoring wild Macaque |
| CN109270564A (en) * | 2018-10-23 | 2019-01-25 | 河南工业职业技术学院 | A kind of high-precision GNSS measuring device and its measurement method |
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2013
- 2013-04-28 CN CN 201320228082 patent/CN203217082U/en not_active Expired - Fee Related
Cited By (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103699133B (en) * | 2013-12-12 | 2016-06-29 | 西安交通大学 | A kind of multi-aircraft lifting coordinated control system |
| CN103699133A (en) * | 2013-12-12 | 2014-04-02 | 西安交通大学 | Multi-aircraft hoisting coordinated control system |
| CN104519314A (en) * | 2013-12-25 | 2015-04-15 | 柳州桂通科技有限公司 | Quick acquisition method of panoramic information of accident site |
| CN104519315A (en) * | 2013-12-25 | 2015-04-15 | 柳州桂通科技有限公司 | Accident scene panoramic information fast collecting device |
| CN104267741A (en) * | 2014-09-12 | 2015-01-07 | 深圳市创新智慧港有限公司 | Aerial photography device with intelligent steering function |
| CN105159318A (en) * | 2015-09-23 | 2015-12-16 | 郑州大学 | Ecological civilization monitoring device and system |
| CN105262986A (en) * | 2015-09-23 | 2016-01-20 | 郑州大学 | Equipment and system for tracing and monitoring wild Macaque |
| CN105204516A (en) * | 2015-09-23 | 2015-12-30 | 郑州大学 | Biological agriculture monitoring method, device and system |
| CN105159318B (en) * | 2015-09-23 | 2018-01-30 | 郑州大学 | Conservation culture monitoring device and system |
| CN105262986B (en) * | 2015-09-23 | 2018-04-10 | 郑州大学 | Wild Macaque tracking monitor apparatus and system |
| CN108153333A (en) * | 2015-09-23 | 2018-06-12 | 郑州大学 | The home port of conservation culture monitoring device |
| CN108227741A (en) * | 2015-09-23 | 2018-06-29 | 郑州大学 | A kind of conservation culture monitors flight instruments |
| CN105204516B (en) * | 2015-09-23 | 2018-12-18 | 郑州大学 | Ecological agriculture monitoring method, apparatus and system |
| CN105242682A (en) * | 2015-11-04 | 2016-01-13 | 北京航天科颐技术有限公司 | Target characteristic measurement system for drone aircraft |
| CN105242682B (en) * | 2015-11-04 | 2018-06-19 | 北京航天科颐技术有限公司 | Target drone target signature measurement system |
| CN109270564A (en) * | 2018-10-23 | 2019-01-25 | 河南工业职业技术学院 | A kind of high-precision GNSS measuring device and its measurement 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: 20130925 Termination date: 20140428 |