CN101746504A - Reconnaissance flight vehicle with infrared distance measuring and hovering function for polices - Google Patents
Reconnaissance flight vehicle with infrared distance measuring and hovering function for polices Download PDFInfo
- Publication number
- CN101746504A CN101746504A CN200810072248A CN200810072248A CN101746504A CN 101746504 A CN101746504 A CN 101746504A CN 200810072248 A CN200810072248 A CN 200810072248A CN 200810072248 A CN200810072248 A CN 200810072248A CN 101746504 A CN101746504 A CN 101746504A
- Authority
- CN
- China
- Prior art keywords
- distance measuring
- infrared distance
- flight vehicle
- unit
- hovering
- 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.)
- Pending
Links
Images
Landscapes
- Traffic Control Systems (AREA)
Abstract
The invention relates to a reconnaissance flight vehicle with an infrared distance measuring and hovering function for polices, comprising a flight vehicle body controlled by a remote controller, the bottom of the flight vehicle is provided with a high-definition charge coupled device (CCD) camera in which a wireless video and audio transmission module wirelessly connected with a video and audio receiver on the ground is arranged, in addition, an infrared distance measuring and fixed-height flight controller is arranged on the flight vehicle; and the controller comprises an infrared transmitting unit for transmitting infrared rays to the ground, a receiving unit for receiving the infrared rays returned from the ground, a phase measuring unit, a counting unit, a logic control unit and an attitude control device for driving the flight device, wherein the phase measuring unit, the counting unit and the logic control unit are communicated for data processing. The reconnaissance flight vehicle is mainly used for reconnoitering or detecting the tendencies of offenders from high altitude on the sites of sudden accidents and transferring the videos of the sites to the headquarters, realizes automatic and fixed-height hovering in the air during fixed-point reconnoitering, is convenient to operate and control and has accurate data and low cost by adopting infrared distance measurement.
Description
Technical field:
The invention belongs to a kind of police and use ferreting device, relate to a kind of reconnaisance flight vehicle, but especially relevant with a kind of alert reconnaisance flight vehicle of using with infrared distance measuring and hovering.
Background technology:
Alert mainly be positioned alertly to use the field, satisfy aerial reconnaissance and patrol, especially anti-terrorism, fire alarm, the patrol police of sudden, zonule etc. with reconnaisance flight vehicle; Can satisfy simultaneously the needs in fields such as the anti-dangerous disaster relief; According to the information that obtains, similar products are applied to 110 patrol police systems abroad, but its product can only artificially be controlled flying height by remote controller, when the fixed point scouting, can't realize that deciding height automatically in the air hovers, the actual inconvenience of using.
Summary of the invention:
The objective of the invention is to solve the aforementioned problems in the prior, a kind of alert reconnaisance flight vehicle of using with infrared distance measuring hovering is provided, be mainly used in the sudden accident scene and scout or survey offender's trend from the high-altitude, transmit the field image data to general headquarters, can realize deciding height in the air and hover automatically.
For reaching above-mentioned purpose, the present invention adopts following technical scheme:
The alert reconnaisance flight vehicle of using of band infrared distance measuring hovering, comprise the aircraft body, described aircraft is controlled by remote controller, its bottom is equiped with the high-resolution ccd video camera, be equiped with wireless image-sound transport module and ground-surface video receiver wireless connections in the pick up camera, on aircraft, be equiped with infrared distance measuring height-lock control controller in addition.
Described infrared distance measuring height-lock control controller comprises: infra-red ray transmitting unit is launched infrared ray earthward, receiving element receives the infrared ray that ground is returned, connection survey facies unit, counting unit, logic control element carry out data handing, drive the attitude-control device of aircraft.
Described aircraft adopts four motor driven, and the screw propeller place is provided with circular arc protection structure.
Adopt technique scheme, the present invention is mainly used in the sudden accident scene and scouts or survey offender's trend from the high-altitude, transmits the field image data to general headquarters, realizes when fixed point is scouted that deciding height automatically in the air hovers, conveniently control, adopt the infrared distance measuring data accurately with low cost.
Description of drawings:
Fig. 1 is a system chart of the present invention;
Fig. 2 is the fixed high control structure figure of infrared distance measuring of the present invention.
The specific embodiment:
Below in conjunction with drawings and Examples the present invention is described in further detail.
Consult shown in Fig. 1-2, the alert reconnaisance flight vehicle of using of band infrared distance measuring hovering, comprise aircraft body 1, described aircraft is by remote controller 4 controls, its bottom is equiped with high-resolution ccd video camera 2, be equiped with wireless image-sound transport module and 5 wireless connections of ground-surface video receiver in the pick up camera 2, on aircraft 1, be equiped with infrared distance measuring height-lock control controller 3 in addition.
Described infrared distance measuring height-lock control controller 3 comprises: infra-red ray transmitting unit 6 is launched infrared ray earthward, receiving element 7 receives the infrared ray that ground is returned, connection survey facies unit 8, counting unit 9, logic control element 10 carry out data handing, drive the attitude-control device of aircraft.
The design of aircraft of the present invention: 1) adopt four motor driven; have a smooth flight; can easily finish various flare maneuvers 2) lithium polymer battery; the time 3 that can fly and reach 45 minutes). screw propeller 11 is respectively equipped with special circular arc protection structure; prevent effectively that blade is impaired, personnel and property escape injury; adopt three-dimensional gyroscope and part of attitude control integrated design, guarantee aerial meticulous location, adopt remote controller to handle control.
Image transmission design: adopt the high-resolution ccd video camera to be installed in the bottom of aircraft, pass real-time video back the ground control point by 2.4G wireless image-sound transport module.
Aerial decide the high controlling Design of hovering automatically: constitute by light modulated (infrared ray) transmitter unit, receiving element, survey facies unit, counting unit, logic control. the real-time measurement of realization distance to the ground, can remote control setting apart from the ground flying height, system realizes deciding the height control of hovering in the air with the automatically regulating flying height and flies.
During work, the aircraft control that will be equipped with four screw propellers by remote controller is taken off, and to the predetermined reconnaissance zone sky, ccd video camera is with the collection in worksite image and send to video receiver so that monitor; When the needs height-lock control, set flying height by remote controller, infrared distance measuring height-lock control controller is started working, by light modulated (infrared ray) transmitter unit launch earthward infrared ray, receiving element receive the infrared ray that returns, by surveying the data handing of facies unit, counting unit, logic controller, the attitude control dress system of direct drive aircraft; Main use alert used the field, satisfies aerial reconnaissance and patrol, especially anti-terrorism, fire alarm, the patrol police of sudden, zonule etc.; Can satisfy simultaneously the needs in fields such as the anti-dangerous disaster relief.
Adopt technique scheme, the present invention is mainly used in the sudden accident scene and scouts or survey offender's trend from the high-altitude, transmits the field image data to general headquarters, realizes when fixed point is scouted that deciding height automatically in the air hovers, conveniently control, adopt the infrared distance measuring data accurately with low cost.
The present invention bases oneself upon sector application, from aircraft itself to flight control system, arrives flight load again, all embodies high reliability, high intelligent characteristics, has powerful technical advantage. By infrared distance measuring, data analysis and setting are realized aircraft auto-flare system height, more according to the interrelated data inquiry, be blank at present.
Claims (3)
1. be with the alert reconnaisance flight vehicle of using of infrared distance measuring hovering, comprise the aircraft body, it is characterized in that: described aircraft is controlled by remote controller, its bottom is equiped with the high-resolution ccd video camera, be equiped with wireless image-sound transport module and ground-surface video receiver wireless connections in the pick up camera, on aircraft, be equiped with infrared distance measuring height-lock control controller in addition.
2. the alert reconnaisance flight vehicle of using of band infrared distance measuring hovering as claimed in claim 1, it is characterized in that: described infrared distance measuring height-lock control controller comprises: infra-red ray transmitting unit is launched infrared ray earthward, receiving element receives the infrared ray that ground is returned, connection survey facies unit, counting unit, logic control element carry out data handing, drive the attitude-control device of aircraft.
3. band infrared distance measuring hovering as claimed in claim 1 or 2 is alert uses reconnaisance flight vehicle, and it is characterized in that: described aircraft adopts four motor driven, and the screw propeller place is provided with circular arc protection structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200810072248A CN101746504A (en) | 2008-12-01 | 2008-12-01 | Reconnaissance flight vehicle with infrared distance measuring and hovering function for polices |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200810072248A CN101746504A (en) | 2008-12-01 | 2008-12-01 | Reconnaissance flight vehicle with infrared distance measuring and hovering function for polices |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101746504A true CN101746504A (en) | 2010-06-23 |
Family
ID=42474271
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN200810072248A Pending CN101746504A (en) | 2008-12-01 | 2008-12-01 | Reconnaissance flight vehicle with infrared distance measuring and hovering function for polices |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101746504A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102514719A (en) * | 2011-12-29 | 2012-06-27 | 广州市阳阳谷信息科技有限公司 | Wireless remote control flying surveillance camera shooting command device |
| CN104180718A (en) * | 2014-07-29 | 2014-12-03 | 北京机械设备研究所 | Localizable remote control flying launching system |
| CN104330803A (en) * | 2014-10-13 | 2015-02-04 | 中国运载火箭技术研究院 | Double-station infrared passive ranging method for maneuverable aircrafts |
| CN104760699A (en) * | 2014-08-28 | 2015-07-08 | 郝恩政 | Manned saucer-shaped aircraft |
| CN104932523A (en) * | 2015-05-27 | 2015-09-23 | 深圳市高巨创新科技开发有限公司 | Positioning method and apparatus for unmanned aerial vehicle |
| CN106872961A (en) * | 2017-04-08 | 2017-06-20 | 北醒（北京）光子科技有限公司 | A kind of optical lens, optical distance measurement apparatus and distance-finding method, range-measurement system |
| WO2018018710A1 (en) * | 2016-07-23 | 2018-02-01 | 深圳曼塔智能科技有限公司 | Unmanned aerial vehicle and flight level control method utilized in unmanned aerial vehicle |
| CN108786011A (en) * | 2016-12-22 | 2018-11-13 | 李峰 | A kind of multi-gym |
-
2008
- 2008-12-01 CN CN200810072248A patent/CN101746504A/en active Pending
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102514719A (en) * | 2011-12-29 | 2012-06-27 | 广州市阳阳谷信息科技有限公司 | Wireless remote control flying surveillance camera shooting command device |
| CN104180718A (en) * | 2014-07-29 | 2014-12-03 | 北京机械设备研究所 | Localizable remote control flying launching system |
| CN104760699A (en) * | 2014-08-28 | 2015-07-08 | 郝恩政 | Manned saucer-shaped aircraft |
| CN104760699B (en) * | 2014-08-28 | 2016-08-24 | 郝恩政 | A kind of manned disc-shaped flying craft |
| CN104330803A (en) * | 2014-10-13 | 2015-02-04 | 中国运载火箭技术研究院 | Double-station infrared passive ranging method for maneuverable aircrafts |
| CN104932523A (en) * | 2015-05-27 | 2015-09-23 | 深圳市高巨创新科技开发有限公司 | Positioning method and apparatus for unmanned aerial vehicle |
| WO2018018710A1 (en) * | 2016-07-23 | 2018-02-01 | 深圳曼塔智能科技有限公司 | Unmanned aerial vehicle and flight level control method utilized in unmanned aerial vehicle |
| CN108786011A (en) * | 2016-12-22 | 2018-11-13 | 李峰 | A kind of multi-gym |
| CN106872961A (en) * | 2017-04-08 | 2017-06-20 | 北醒（北京）光子科技有限公司 | A kind of optical lens, optical distance measurement apparatus and distance-finding method, range-measurement system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11407526B2 (en) | Systems and methods for UAV docking | |
| CN101746504A (en) | Reconnaissance flight vehicle with infrared distance measuring and hovering function for polices | |
| CN201334116Y (en) | Hovering police reconnaissance flight vehicle with infra-red range measuring function | |
| KR101933402B1 (en) | A wired drone system which communicates wirelessly and can fly for a long period of time | |
| CN107585222B (en) | Unmanned reconnaissance vehicle | |
| EP1767453B1 (en) | Autonomous launch pad for micro air vehicles | |
| CN206485574U (en) | A kind of remote highway rescue system based on unmanned aerial vehicle platform | |
| CN201364497Y (en) | Remote-control far-distance monitoring and loading unmanned helicopter system | |
| CN105551280A (en) | Unmanned aerial vehicle traffic signal indicating system | |
| CN105059550A (en) | Double unmanned aerial vehicle with improved endurance | |
| CN107037845A (en) | One kind is taken photo by plane UAV Flight Control System | |
| CN104816829B (en) | Skyeye aircraft applicable to investigation | |
| CN107942348B (en) | Road law enforcement system based on unmanned aerial vehicle and robot technique | |
| CN101746503A (en) | Police reconnaissance aircraft with GPS positioning missile | |
| CN205931243U (en) | Alert unmanned aerial vehicle that uses | |
| US20230176566A1 (en) | Wireless communication system of intelligent uav | |
| CN108803633A (en) | A kind of unmanned plane low latitude monitoring system based on mobile communications network | |
| CN105549494A (en) | Automobile and unmanned aerial vehicle connecting device | |
| CN205959071U (en) | Unmanned aerial vehicle landing bootstrap system | |
| CN205131675U (en) | Intelligence unmanned aerial vehicle system based on long -range target of listening of infrared ray | |
| KR20230121479A (en) | Remote Monitoring System using Tethered Drone Station using the same | |
| KR102441077B1 (en) | Apparatus for controlling taking off and landing of a dron in a vehicle and method thereof | |
| CN105760853A (en) | Personnel flow monitoring unmanned aerial vehicle | |
| CN214174919U (en) | A rotor unmanned aerial vehicle cluster system for burning explodes calamity early warning and processing | |
| CN109383798A (en) | A kind of vehicle-mounted police UAV system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Open date: 20100623 |