CN201334116Y - Hovering police reconnaissance flight vehicle with infra-red range measuring function - Google Patents
Hovering police reconnaissance flight vehicle with infra-red range measuring function Download PDFInfo
- Publication number
- CN201334116Y CN201334116Y CNU2008202291887U CN200820229188U CN201334116Y CN 201334116 Y CN201334116 Y CN 201334116Y CN U2008202291887 U CNU2008202291887 U CN U2008202291887U CN 200820229188 U CN200820229188 U CN 200820229188U CN 201334116 Y CN201334116 Y CN 201334116Y
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- 208000035126 Facies Diseases 0.000 claims description 5
- 230000005540 biological transmission Effects 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
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Abstract
The utility model relates to a hovering police reconnaissance flight vehicle with infra-red range measuring function, which comprises a flight vehicle body, wherein the flight vehicle is controlled by a remote control, and a high-definition CCD camera is installed at the bottom of the flight vehicle; a wireless audio-visual transmission module which is installed in the camera is wirelessly connected with a ground image receiver, and an infra-red range measuring constant-level flight controller is installed on the flight vehicle; the controller comprises an infrared emission unit, a receiving unit, a phase measuring unit, a counting unit and a logic control unit; and the infrared emission unit emits infrared rays to the ground, and the receiving unit receives the ground-returned infrared rays which directly drive the attitude control device of the flight vehicle through the digital processing of the phase measuring unit, the counting unit and the logic control unit. The utility model is mainly used for observing or detecting criminal trends from the high-altitude at the scenes of sudden accidents to send scene image data to the headquarters, realizes the automatic constant-level hovering during the pinpoint reconnaissance, facilitates the control, and has accurate infra-red range measuring data and low cost.
Description
Technical field:
The utility model belongs to the utility model and belongs to a kind of and alert use ferreting device, relates to a kind of reconnaisance flight vehicle, but especially with a kind of alert relevant with infrared distance measuring and hovering with reconnaisance flight vehicle.
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.
The utility model content:
The purpose of this utility model 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 utility model 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 utility model 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 utility model;
Fig. 2 is the fixed high control structure figure of infrared distance measuring of the present utility model.
The specific embodiment:
Below in conjunction with drawings and Examples the utility model 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 the utility model aircraft: 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 utility model 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 utility model bases oneself upon sector application, to flight control system, arrives flight load from aircraft itself again, all embodies high reliability, high intelligent characteristics, has powerful technical advantage.By infrared distance measuring, realization aircraft auto-flare system height is analyzed and set to data, more according to the pertinent data inquiry, be blank at present.
Claims (3)
1, the alert reconnaisance flight vehicle of using of band 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 |
|---|---|---|---|
| CNU2008202291887U CN201334116Y (en) | 2008-12-01 | 2008-12-01 | Hovering police reconnaissance flight vehicle with infra-red range measuring function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008202291887U CN201334116Y (en) | 2008-12-01 | 2008-12-01 | Hovering police reconnaissance flight vehicle with infra-red range measuring function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201334116Y true CN201334116Y (en) | 2009-10-28 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2008202291887U Expired - Fee Related CN201334116Y (en) | 2008-12-01 | 2008-12-01 | Hovering police reconnaissance flight vehicle with infra-red range measuring function |
Country Status (1)
| Country | Link |
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| CN (1) | CN201334116Y (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103144770A (en) * | 2013-03-19 | 2013-06-12 | 南京航空航天大学 | Full-automatic indoor environment control, obstacle avoidance and navigation type micro aerial vehicle |
| CN104157165A (en) * | 2014-08-11 | 2014-11-19 | 江苏恒创软件有限公司 | Unmanned helicopter-based urban area motor vehicle parking planning method |
| CN104180718A (en) * | 2014-07-29 | 2014-12-03 | 北京机械设备研究所 | Localizable remote control flying launching system |
| CN105491330A (en) * | 2015-11-25 | 2016-04-13 | 深圳市龙云创新航空科技有限公司 | Unmanned aerial vehicle system and air battle method thereof |
| CN106043693A (en) * | 2016-06-14 | 2016-10-26 | 河南华泰规划勘测设计咨询有限公司 | Unmanned aerial vehicle for surveying and mapping |
| CN107656529A (en) * | 2016-07-23 | 2018-02-02 | 深圳曼塔智能科技有限公司 | Unmanned plane and the fixed high control method of unmanned plane |
| CN108974375A (en) * | 2018-07-16 | 2018-12-11 | 河南聚合科技有限公司 | A kind of hybrid power land, water and air three, which are dwelt, unmanned scouts identification percussion system |
-
2008
- 2008-12-01 CN CNU2008202291887U patent/CN201334116Y/en not_active Expired - Fee Related
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103144770A (en) * | 2013-03-19 | 2013-06-12 | 南京航空航天大学 | Full-automatic indoor environment control, obstacle avoidance and navigation type micro aerial vehicle |
| CN103144770B (en) * | 2013-03-19 | 2015-10-28 | 南京航空航天大学 | A kind of entirely keep away barrier navigation minute vehicle from master control environment of entering the room |
| CN104180718A (en) * | 2014-07-29 | 2014-12-03 | 北京机械设备研究所 | Localizable remote control flying launching system |
| CN104157165A (en) * | 2014-08-11 | 2014-11-19 | 江苏恒创软件有限公司 | Unmanned helicopter-based urban area motor vehicle parking planning method |
| CN104157165B (en) * | 2014-08-11 | 2016-07-06 | 江苏恒创软件有限公司 | A kind of urban area motor vehicle parking planing method based on unmanned plane |
| CN105491330A (en) * | 2015-11-25 | 2016-04-13 | 深圳市龙云创新航空科技有限公司 | Unmanned aerial vehicle system and air battle method thereof |
| CN106043693A (en) * | 2016-06-14 | 2016-10-26 | 河南华泰规划勘测设计咨询有限公司 | Unmanned aerial vehicle for surveying and mapping |
| CN107656529A (en) * | 2016-07-23 | 2018-02-02 | 深圳曼塔智能科技有限公司 | Unmanned plane and the fixed high control method of unmanned plane |
| CN108974375A (en) * | 2018-07-16 | 2018-12-11 | 河南聚合科技有限公司 | A kind of hybrid power land, water and air three, which are dwelt, unmanned scouts identification percussion system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee |
Owner name: LUOPUTE (XIAMEN) TECHNOLOGY GROUP CO., LTD. Free format text: FORMER NAME: XIAMEN ROPEOK SCIENCE AND TECHNOLOGY CO., LTD. |
|
| CP03 | Change of name, title or address |
Address after: 361000, Fujian, Xiamen torch hi tech Zone (Xiangan) Industrial Zone, 69 Yue Xiang Road, three Southeast Patentee after: Ropt (Xiamen) Technology Group Co., Ltd. Address before: 361000, Fujian, Huli District, Xiamen Province Torch hi tech Zone (Xiangan) Industrial Zone, 69 Yue Xiang Road, three Southeast Patentee before: Xiamen ROPEOK Science and Technology Co., Ltd. |
|
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20091028 Termination date: 20171201 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |