CN204173162U - Based on the vehicular photoelectric reconnaissance system of multi-rotor aerocraft - Google Patents
Based on the vehicular photoelectric reconnaissance system of multi-rotor aerocraft Download PDFInfo
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- CN204173162U CN204173162U CN201420498646.2U CN201420498646U CN204173162U CN 204173162 U CN204173162 U CN 204173162U CN 201420498646 U CN201420498646 U CN 201420498646U CN 204173162 U CN204173162 U CN 204173162U
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- 238000001514 detection method Methods 0.000 claims abstract description 16
- 230000000087 stabilizing effect Effects 0.000 claims abstract description 15
- 230000005540 biological transmission Effects 0.000 claims abstract description 5
- 230000004297 night vision Effects 0.000 claims description 2
- 238000001931 thermography Methods 0.000 claims description 2
- 230000003287 optical effect Effects 0.000 abstract 1
- 238000000034 method Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000000007 visual effect Effects 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical group C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000005622 photoelectricity Effects 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
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Abstract
The utility model provides the vehicular photoelectric reconnaissance system based on multi-rotor aerocraft, and this system comprises: carry car, multi-rotor aerocraft, stabilizing device, navigational aid, photoelectronic reconnaissance equipment and connecting cable.Aircraft carries out electric power and data transmission with a year workshop by being connected to the cable that can depart from socket.When needing, connecting cable can automatically disengage with aircraft, performs the reconnaissance mission approaching target.Being installed on stabilizing device on multi-rotor aerocraft for photoelectronic reconnaissance equipment provides stable working environment, the photoelectronic reconnaissance equipment detection of a target combine with navigational aid, provide target image data to be measured and absolute location coordinates data.Compared with existing vehicle mounted mast formula electro optical reconnaissance system, the utility model by the impact of ground obstacle and surface conditions, is not more suitable for the running dynamic instrumentation of vehicle, and aircraft can automatically disengage and carries a car and carry out proximity detection to the detection of a target.
Description
Technical field
This practicality belongs to electronic reconnaissance field, particularly a kind of vehicular photoelectric reconnaissance system.
Background technology
Vehicular photoelectric reconnaissance system can be caught rapidly, tracking and aiming target, in recent years except obtaining except widespread use on weapon guidance, firepower control, also in commercialization relief, the condition of a disaster is anti-to be rescued, and frontier defense anti-smuggling etc. needs the field of target positioning or Target indication to obtain important application.
For making sensor have the openr visual field, avoiding the ground low obstacles such as trees blocking sensor, expanding and scouting search coverage, general photoelectronic reconnaissance equipment is all arranged on the liftable mast of year car now.But in the process of carrying car motion, due to factor impacts such as road surfaces, the shaking volume of mast is imponderable, can cause imponderable impact to precision, carries out detecting when therefore masts type vehicular photoelectric reconnaissance system is all stationary vehicle at present.In addition for the region that year car cannot arrive at, proximity detection cannot be carried out to the detection of a target.
Utility model content
For the deficiency of aforementioned system, the utility model provides a kind of vehicular photoelectric reconnaissance system based on multi-rotor aerocraft, to carry in car driving process, and also can accurate detection target or region cannot be arrived at also can closely observe carrying a car.
In order to achieve the above object, the utility model takes following technical scheme:
Based on a vehicular photoelectric reconnaissance system for multi-rotor aerocraft, comprise and carry car, multi-rotor aerocraft, stabilizing device, navigational aid, photoelectronic reconnaissance equipment and connecting cable; Wherein, described stabilizing device hangs on aircraft, and photoelectronic reconnaissance equipment is installed on stabilizing device, and stabilizing device provides stable working environment for photoelectronic reconnaissance equipment; Described navigational aid is installed on aircraft, and by navigational aid and photoelectronic reconnaissance equipment, system provides position and the image data of target to be measured for user; Described aircraft transmits detection data by cable to carrying car, or wirelessly carries car transmission detection data earthward; Within described year, car comprises control desk and read out instrument, and within described year, car is manipulated aircraft and reconnaissance equipment by wired or wireless mode.
Further, described photoelectronic reconnaissance equipment comprises one or more in laser rangefinder, camera, pick up camera, infrared thermography and low-light level night vision device.
Further, described stabilizing device comprises damper mechanism and stable platform, or only comprises damper mechanism.Described stable platform is diaxon or three gyroplatform.
Further, described multi-rotor aerocraft rotor quantity is four rotors, six rotors, eight rotors or 16 rotors.
Further, described navigational aid comprises one or more in gyro, accelerometer, navigational satellite receiver, magnetometer.
Further, within described year, car is powered to aircraft by cable, or the battery-operated aircraft carried by aircraft and reconnaissance equipment work.
Further, described aircraft and carry car cable and is connected by can depart from socket, if desired, cable departs from aircraft automatically, thus is convenient to aircraft disengaging year car and fetters and detect target.
The beneficial effects of the utility model are: the vehicular photoelectric reconnaissance system based on multi-rotor aerocraft of the present utility model, and aircraft carries out electric power and data transmission with a year workshop by being connected to the cable that can depart from socket.Aircraft also can depart from a year car cable and be connected, and relies on the battery of self to provide electric power, by wireless link to carrying a car returned data.When needing, connecting cable can automatically disengage with aircraft, performs the reconnaissance mission approaching target.Stabilizing device is connected with aircraft by damper mechanism, for photoelectronic reconnaissance equipment provides stable working environment.By the luffing angle of telecommand equipment adjustment stable platform, course heading, facilitates different visual angles to detect.Pick up camera and infrared thermoviewer can obtain target image, and laser rangefinder can record the oblique distance of aircraft and the detection of a target, merge mutually, system just can provide target image data to be measured and absolute location coordinates data with the navigation data of reconnaissance system self.Be sent to through cable or wireless link and carry car reception facilities, for showing in real time.Make carrying in car driving process, accurate detection target or region cannot be arrived at also can closely observe carrying a car, for the region of carrying car and cannot arrive at, also can carry out proximity detection to the detection of a target.
Accompanying drawing explanation
Fig. 1 is the composition diagram of vehicular photoelectric reconnaissance system of the present utility model;
Fig. 2 is the functional block diagram of vehicular photoelectric reconnaissance system of the present utility model.
Detailed description of the invention
To illustrate below in conjunction with accompanying drawing and detailed description of the invention further illustrates the utility model.
As shown in Figure 1, the vehicular photoelectric reconnaissance system based on multi-rotor aerocraft of the present utility model, comprises and carries car subsystem and flight subsystem.As shown in Figure 2, the read out instrument of the control setup being provided with aircraft in car 1 and display reconnaissance data is carried.Flight subsystem comprises the homing advice on aircraft 5 top and flight control unit 2 and is positioned at stabilizing device (comprising damper mechanism and stable platform 3) and the photoelectronic reconnaissance equipment 4 of aircraft bottom.Carry car to be connected by being connected to the cable 6 automatically disengaged on adaptor union with aircraft.Described stable platform is two axis gyroscope stable platform; Described photoelectricity investigation equipment comprises laser rangefinder, infrared thermoviewer, pick up camera; Described homing advice comprises three axis magnetometer, triaxial accelerometer, three axle gyros and BD/GPS receiver etc.; Described flight controller can be made up of the embedded device such as micro controller system, ARM.
Aircraft is mounted at ordinary times and carries on car, with carrying car motion.When needing detection, moved through cable or wireless spread-spectrum technology aircraft vertical by control setup by operator, rise to specified altitude assignment, aircraft hovers, and reconnaissance equipment is scouted intended target.Damper mechanism can isolate body vibration, operator can control stable platform azimuth axis in N × 360 ° scope, pitch axis is rotation sweep in 0 ~ 90 °.The view data of target is obtained by pick up camera or infrared thermoviewer, the position data of target is settled accounts through data anastomosing algorithm by laser rangefinder and homing advice, the destination image data obtained and position data pass under cable or wireless link carries car, is shown in real time by read out instrument.Carry car when needs aircraft departs from, when carrying out careful scouting to target, operating personal sends instruction, automatically disengages adaptor union and cable is separated with aircraft.At this moment aircraft is provided by its cells, carries the target image and location information etc. that the up control command of truck control device and aircraft pass down, complete the detection to target by transmission of radio links.
Above content is in conjunction with concrete preferred implementation further detailed description of the utility model, can not assert that concrete enforcement of the present utility model is confined to these explanations.For the utility model person of an ordinary skill in the technical field, without departing from the concept of the premise utility, some simple deduction or replace can also be made, all should be considered as belonging to protection domain of the present utility model.
Claims (8)
1. based on a vehicular photoelectric reconnaissance system for multi-rotor aerocraft, it is characterized in that: described system comprises carries car, multi-rotor aerocraft, stabilizing device, navigational aid, photoelectronic reconnaissance equipment and connecting cable; Wherein, described stabilizing device hangs on aircraft, and photoelectronic reconnaissance equipment is installed on stabilizing device, and stabilizing device provides stable working environment for photoelectronic reconnaissance equipment; Described navigational aid is installed on aircraft, and by navigational aid and photoelectronic reconnaissance equipment, system provides position and the image data of target to be measured for user; Described aircraft transmits detection data by cable to carrying car, or wirelessly carries car transmission detection data earthward; Within described year, car comprises control desk and read out instrument, and within described year, car is manipulated aircraft and reconnaissance equipment by wired or wireless mode.
2. system according to claim 1, is characterized in that: described photoelectronic reconnaissance equipment comprise in laser rangefinder, camera, pick up camera, infrared thermography and low-light level night vision device one or more.
3. system according to claim 1, is characterized in that: described stabilizing device comprises damper mechanism and stable platform, or only comprises damper mechanism.
4. system according to claim 1, is characterized in that: described stabilizing device comprises damper mechanism and stable platform, and described stable platform is diaxon or three gyroplatform.
5. system according to claim 1, is characterized in that: described multi-rotor aerocraft rotor quantity is four rotors, six rotors, eight rotors or 16 rotors.
6. system according to claim 1, is characterized in that: described navigational aid comprise in gyro, accelerometer, navigational satellite receiver, magnetometer one or more.
7. system according to claim 1, is characterized in that: within described year, car is powered to aircraft by cable, or the battery-operated aircraft carried by aircraft and reconnaissance equipment work.
8. system according to claim 1, is characterized in that: described aircraft and carry car cable and is connected by can depart from socket, and if desired, cable departs from aircraft automatically, thus is convenient to aircraft disengaging year car and fetters and detect target.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420498646.2U CN204173162U (en) | 2014-09-01 | 2014-09-01 | Based on the vehicular photoelectric reconnaissance system of multi-rotor aerocraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420498646.2U CN204173162U (en) | 2014-09-01 | 2014-09-01 | Based on the vehicular photoelectric reconnaissance system of multi-rotor aerocraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204173162U true CN204173162U (en) | 2015-02-25 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420498646.2U Expired - Lifetime CN204173162U (en) | 2014-09-01 | 2014-09-01 | Based on the vehicular photoelectric reconnaissance system of multi-rotor aerocraft |
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Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104889997A (en) * | 2015-07-03 | 2015-09-09 | 四川理工学院 | Solid brewing yeast turning precisely-positioned mechanical hand control system and method |
| CN106101657A (en) * | 2016-08-10 | 2016-11-09 | 山东神戎电子股份有限公司 | A kind of laser night vision monitoring system based on multi-rotor aerocraft |
| CN106218879A (en) * | 2016-08-23 | 2016-12-14 | 上海牧羽航空科技有限公司 | A kind of split type low clearance manned vehicle |
| CN106292684A (en) * | 2015-05-13 | 2017-01-04 | 日立(中国)研究开发有限公司 | Carry the vehicle of aircraft |
| CN106274626A (en) * | 2016-08-31 | 2017-01-04 | 杨静宇 | The ground robot of variable field of view height |
| CN106628134A (en) * | 2015-10-28 | 2017-05-10 | 顾晓伟 | Rotor flight apparatus and control method thereof |
| CN106985765A (en) * | 2017-04-25 | 2017-07-28 | 苏州科伊嘉航空科技有限公司 | One kind has wing aircraft vehicle mounted imaging apparatus |
| CN108227733A (en) * | 2017-11-30 | 2018-06-29 | 国网河南省电力公司偃师市供电公司 | A kind of method and apparatus of insulation fault location in ungrounded electric power system |
| CN111392039A (en) * | 2020-03-18 | 2020-07-10 | 浙江吉利汽车研究院有限公司 | Auxiliary control system and control method for car lamp |
| CN111806685A (en) * | 2020-06-23 | 2020-10-23 | 亚投中财(北京)科技开发有限公司 | Green photoelectric sensing system for integrated application of suspension type vehicle-mounted three-dimensional monitoring aircraft |
-
2014
- 2014-09-01 CN CN201420498646.2U patent/CN204173162U/en not_active Expired - Lifetime
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106292684A (en) * | 2015-05-13 | 2017-01-04 | 日立(中国)研究开发有限公司 | Carry the vehicle of aircraft |
| CN104889997A (en) * | 2015-07-03 | 2015-09-09 | 四川理工学院 | Solid brewing yeast turning precisely-positioned mechanical hand control system and method |
| CN106628134B (en) * | 2015-10-28 | 2019-11-05 | 顾晓伟 | A kind of rotor flight device and its control method |
| CN106628134A (en) * | 2015-10-28 | 2017-05-10 | 顾晓伟 | Rotor flight apparatus and control method thereof |
| CN106101657A (en) * | 2016-08-10 | 2016-11-09 | 山东神戎电子股份有限公司 | A kind of laser night vision monitoring system based on multi-rotor aerocraft |
| CN106218879A (en) * | 2016-08-23 | 2016-12-14 | 上海牧羽航空科技有限公司 | A kind of split type low clearance manned vehicle |
| CN106218879B (en) * | 2016-08-23 | 2018-05-01 | 上海牧羽航空科技有限公司 | A kind of split type low clearance manned vehicle |
| CN106274626A (en) * | 2016-08-31 | 2017-01-04 | 杨静宇 | The ground robot of variable field of view height |
| CN106985765A (en) * | 2017-04-25 | 2017-07-28 | 苏州科伊嘉航空科技有限公司 | One kind has wing aircraft vehicle mounted imaging apparatus |
| CN108227733A (en) * | 2017-11-30 | 2018-06-29 | 国网河南省电力公司偃师市供电公司 | A kind of method and apparatus of insulation fault location in ungrounded electric power system |
| CN111392039A (en) * | 2020-03-18 | 2020-07-10 | 浙江吉利汽车研究院有限公司 | Auxiliary control system and control method for car lamp |
| CN111392039B (en) * | 2020-03-18 | 2021-11-16 | 浙江吉利汽车研究院有限公司 | Auxiliary control system and control method for car lamp |
| CN111806685A (en) * | 2020-06-23 | 2020-10-23 | 亚投中财(北京)科技开发有限公司 | Green photoelectric sensing system for integrated application of suspension type vehicle-mounted three-dimensional monitoring aircraft |
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Legal Events
| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: 518000 whole building of satellite building, 61 Gaoxin South Jiudao, Yuehai street, Nanshan District, Shenzhen City, Guangdong Province Patentee after: Shenzhen Aerospace Dongfanghong Satellite Co.,Ltd. Address before: 518057 room 910, block D, Shenzhen Institute of space technology innovation, South 10th Road, Science Park, Nanshan District, Shenzhen City, Guangdong Province Patentee before: AEROSPACE DONGFANGHONG DEVELOPMENT Ltd. |
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| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20150225 |