CN104180718A - Localizable remote control flying launching system - Google Patents
Localizable remote control flying launching system Download PDFInfo
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- CN104180718A CN104180718A CN201410364568.1A CN201410364568A CN104180718A CN 104180718 A CN104180718 A CN 104180718A CN 201410364568 A CN201410364568 A CN 201410364568A CN 104180718 A CN104180718 A CN 104180718A
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- remote control
- flying platform
- control system
- transceiving device
- camera
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Abstract
The invention discloses a localizable remote control flying launching system which comprises a flying platform (1), a message receiving and sending device (2), a camera (3), a remote control system (6), a distance measuring device (4), a launcher (5) and position calibration devices (7), wherein the message receiving and sending device (2), the camera (3), the distance measuring device (4) and the launcher (5) are arranged on the flying platform (1); the flying platform (1) determines position coordinates through a plurality of position calibration devices (7) arranged on the edge of a set area in a dispersing manner, the remote control system (6) is responsible for locking a shooting target of the launcher (5) in flight, calculating the position coordinates and issuing a launching instruction, and finally, the launcher (5) launches ammunition to the shooting target. The system is suitable for controlling a plurality of occasions by a few people, and when a sudden violent accident happens in the control occasions, the launcher can accurately and rapidly reach the violence burst location to stop the violence.
Description
Technical field
The present invention relates to a kind of remote control distributor emission system, particularly one can remote position controlled flight emission system.
Background technology
Have at present the remote control distributor device with camera, can be in remote control distributor process non-at-scene Real Time Observation target.The existing remote control distributor emission system with camera, comprising: flying platform, information transceiving device, camera and remote control system.Do not possess accurate positioning function and take as required the ability of transmitting action.
Summary of the invention
The object of the invention be to provide one can remote position controlled flight emission system, solve the problem that remote control distributor emission system does not possess accurate positioning function and takes as required transmitting action.
One can remote position controlled flight emission system, comprising: flying platform, information transceiving device, camera and remote control system, also comprise: range unit, emitter and position label means.
Information transceiving device, camera, range unit and emitter are placed on flying platform and are connected by screw, and flying platform, camera, range unit and emitter are connected by cable with information transceiving device respectively, realize electrical interconnection and communication.Multiple position label means disperse to be placed on the edge of setting regions, and remote control system is placed separately.
Use this can remote position controlled when flight emission system, remote control system sends control instruction information, the information transceiving device on flying platform receives after instruction, controls flying platform and takes off.In flight course, the multiple position label means that are placed on setting regions edge are sent wireless position demarcation signal, information transceiving device on flying platform receives after location position signal, determine the position coordinate value of flying platform in this setting regions, and position coordinate value is sent to remote control system in real time.The real-time pictures that camera on flying platform is taken is dealt into remote control system by information transceiving device, effector is by real-time pictures object observing situation, and lock onto target, range unit is dealt into remote control system flying platform apart from the distance value of target by information transceiving device simultaneously, and remote control system calculates the position coordinate value of target.Remote control system provides transmitting whether information according to the position coordinate value of flying platform and target, when after remote control system prompting transmitting, effector assigns firing order information, and firing order information exchange is crossed after information transceiving device reception, controls emitter transmitting ammunition target.
Native system is applicable to the multiple places of a small amount of personnel's centralized management, in the time of management and control place burst incident of violence, utilizes this device at the scene of awaiting orders in advance, accurately arrives fast violence burst point, and the continuation that stops violence is implemented.
Brief description of the drawings
Fig. 1 a kind of can remote position controlled the structural representation of flight emission system.
1. flying platform 2. information transceiving device 3. camera 4. range unit 5. emitter 6. remote control system 7. position label means.
Detailed description of the invention
One can remote position controlled flight emission system, comprising: flying platform 1, information transceiving device 2, camera 3, remote control system 6, also comprise range unit 4, emitter 5, position label means 7.
Information transceiving device 2, camera 3, range unit 4 and emitter 5 are placed on flying platform 1 and are connected by screw, flying platform 1, camera 3, range unit 4 and emitter 5 are connected to information transceiving device 2 by cable respectively, realize electrical interconnection and communication.Multiple position label means 7 disperse to be placed on the edge of setting regions, and remote control system 6 is placed separately.
Use this can remote position controlled when flight emission system, remote control system 6 sends control instruction information, the information transceiving device 2 on flying platform 1 receives after instruction, controls flying platform 1 and takes off.In flight course, the multiple position label means 7 that are placed on setting regions edge are sent wireless position demarcation signal, information transceiving device 2 on flying platform 1 receives after location position signal, can determine the position coordinate value of flying platform 1 in this setting regions, and position coordinate value is sent to remote control system 6 in real time.The real-time pictures that camera 3 on flying platform 1 is taken is dealt into remote control system 6 by information transceiving device 2, effector can pass through real-time pictures object observing situation, and lock onto target, range unit 4 is dealt into remote control system 6 flying platform apart from the distance value of target by information transceiving device 2 simultaneously, and remote control system 6 can calculate the position coordinate value of target.Remote control system 6 provides and whether launches information according to the position coordinate value of flying platform 1 and target, when after remote control system 6 prompting transmittings, effector assigns firing order information, firing order information exchange is crossed after information transceiving device 2 receptions, controls emitter 5 and launches ammunition target.
Claims (1)
- One kind can remote position controlled flight emission system, comprise: flying platform (1), information transceiving device (2), camera (3) and remote control system (6), characterized by further comprising: range unit (4), emitter (5) and position label means (7);Information transceiving device (2), camera (3), range unit (4) and emitter (5) are placed in flying platform (1) and go up and be connected by screw, flying platform (1), camera (3), range unit (4) and emitter (5) are connected by cable with information transceiving device (2) respectively, realize electrical interconnection and communication; Multiple position label means (7) disperse to be placed on the edge of setting regions, and remote control system (6) is placed separately;Use this can remote position controlled when flight emission system, remote control system (6) sends control instruction information, the information transceiving device (2) on flying platform (1) receives after instruction, controls flying platform (1) and takes off; In flight course, the multiple position label means (7) that are placed on setting regions edge are sent wireless position demarcation signal, information transceiving device (2) on flying platform (1) receives after location position signal, determine the position coordinate value of flying platform (1) in this setting regions, and position coordinate value is sent to remote control system (6) in real time; The real-time pictures that camera (3) on flying platform (1) is taken is dealt into remote control system (6) by information transceiving device (2), effector is by real-time pictures object observing situation, and lock onto target, range unit (4) is dealt into remote control system (6) flying platform (1) apart from the distance value of target by information transceiving device (2) simultaneously, and remote control system (6) calculates the position coordinate value of target; Remote control system (6) provides transmitting whether information according to the position coordinate value of flying platform (1) and target, when after remote control system (6) prompting transmitting, effector assigns firing order information, firing order information exchange is crossed after information transceiving device (2) reception, controls emitter (5) transmitting ammunition target.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410364568.1A CN104180718A (en) | 2014-07-29 | 2014-07-29 | Localizable remote control flying launching system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410364568.1A CN104180718A (en) | 2014-07-29 | 2014-07-29 | Localizable remote control flying launching system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104180718A true CN104180718A (en) | 2014-12-03 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410364568.1A Pending CN104180718A (en) | 2014-07-29 | 2014-07-29 | Localizable remote control flying launching system |
Country Status (1)
| Country | Link |
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| CN (1) | CN104180718A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN109035737A (en) * | 2018-08-31 | 2018-12-18 | 西安航天动力技术研究所 | A kind of wireless transmission control system based on ZigBee technology |
| CN110500916A (en) * | 2019-07-22 | 2019-11-26 | 六安智华工业自动化技术有限公司 | A kind of system of the pesticide grown of semi-automation |
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| CN202221475U (en) * | 2011-07-26 | 2012-05-16 | 上海交通大学 | System device for positioning and flight track recording of miniature aircraft |
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Patent Citations (8)
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| JP2002362497A (en) * | 2001-06-11 | 2002-12-18 | Nec Corp | Simple flight control system for unmanned aircraft, on- board flight control device and ground/ship-board simple flight control device |
| CN201334116Y (en) * | 2008-12-01 | 2009-10-28 | 厦门市罗普特科技有限公司 | Hovering police reconnaissance flight vehicle with infra-red range measuring function |
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| CN102348996A (en) * | 2009-02-16 | 2012-02-08 | 空中客车营运有限公司 | Sensors for an aircraft for locating devices |
| CN101881819A (en) * | 2009-05-08 | 2010-11-10 | 刘伯安 | Radio navigation method and/or network and application |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109035737A (en) * | 2018-08-31 | 2018-12-18 | 西安航天动力技术研究所 | A kind of wireless transmission control system based on ZigBee technology |
| CN110500916A (en) * | 2019-07-22 | 2019-11-26 | 六安智华工业自动化技术有限公司 | A kind of system of the pesticide grown of semi-automation |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20141203 |