CN103531044A - Barrier alarm system for unmanned aerial vehicle - Google Patents
Barrier alarm system for unmanned aerial vehicle Download PDFInfo
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- CN103531044A CN103531044A CN201310480659.7A CN201310480659A CN103531044A CN 103531044 A CN103531044 A CN 103531044A CN 201310480659 A CN201310480659 A CN 201310480659A CN 103531044 A CN103531044 A CN 103531044A
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Abstract
The invention relates to a flight control system for an unmanned aerial vehicle, in particular to a barrier alarm system for the unmanned aerial vehicle. The barrier alarm system comprises an airborne end and a control console end, wherein the airborne end comprises a range sensor, the range sensor is connected with a controller, and the controller is connected with an airborne wireless communication module; the control console end comprises a local wireless communication module, the local wireless communication module is connected with an early warning controller, and the early warning controller is connected with an early warning prompt module. According to the barrier alarm system for the unmanned aerial vehicle, the range sensor monitors whether a barrier exists in the front or not in the flying process, when the barrier exists, the early warning information is transmitted by the airborne wireless communication module to the control console end, the control console end receives a signal and carries out early warning prompt, an operator can adjust the flying state of the unmanned aerial vehicle to prevent the unmanned aerial vehicle from colliding with a barrier to cause loss.
Description
Technical field
The present invention relates to a kind of UAV Flight Control System, especially a kind of unmanned plane obstruction warning system.
Background technology
Unmanned spacecraft is called for short " unmanned plane ", is the not manned aircraft that utilizes radio robot and the presetting apparatus of providing for oneself to handle.On machine, without driving cabin, but the equipment such as robot pilot, presetting apparatus are installed.On ground, naval vessels or machine tool remote-controlled station personnel by equipment such as radars, to its follow the tracks of, location, remote control, remote measurement and digital transmission.Can under wireless remote control, as conventional airplane, take off or launch with booster rocket, also can take aerial input to by machine tool and fly.During recovery, the available mode automatic Landing the same with conventional airplane landing mission, also can reclaim with parachute or block by remote control.
The control of existing unmanned plane generally has two kinds, a kind of is automatically to control, a kind of is manually to control, wherein most the use manually of civil small-scale unmanned plane controlled, and by a control desk, the flight of unmanned plane operated, due to limited conditions, aircraft is in flight course, because misoperation or physical features such as are unfamiliar with at the reason, after unmanned plane execution error instruction, likely cause danger, cause damage.
Summary of the invention
The invention provides a kind of unmanned plane obstruction warning system that can carry out obstruction forewarning to operating personnel, prevent maloperation.
To achieve these goals, the present invention adopts following technical scheme:
Comprise airborne end and control you, described airborne end comprises a range sensor, and described range sensor connects a controller, and controller connects an airborne wireless communication module; Described control you comprises a local wireless communication module, and described local wireless communication module connects an early warning controller, and early warning controller is connected with early warning module.
Preferably, described range sensor is located at front fuselage.
Preferably, described early warning module comprises acousto-optic warning unit.
Preferably, described early warning module involving vibrations Tip element also.
Preferably, described acousto-optic hint unit comprises pilot lamp and loudspeaker.
Preferably, described pilot lamp is LED light.
Preferably, described LED light comprises the blue tri-colour LED of reddish yellow.
Preferably, described vibration prompt unit is a vibrating motor.
Preferably, described airborne wireless communication module is 3G communication module.
Preferably, described local wireless communication module is 3G communication module.
Owing to having adopted said structure, whether unmanned plane obstruction warning system of the present invention has barrier in flight course middle distance Sensor monitoring the place ahead, when having barrier, by airborne wireless communication module, early warning information is sent to control you, early warning is carried out in the collection of letters number of control desk termination later, operating personnel can adjust the state of flight of unmanned plane, to avoid unmanned aerial vehicle to cause damage to barrier.
Accompanying drawing explanation
Fig. 1 is the airborne end modular structure schematic diagram of the embodiment of the present invention;
Fig. 2 is the control you modular structure schematic diagram of the embodiment of the present invention.
Embodiment
As shown in Figure 1-2, the unmanned plane obstruction warning system of the present embodiment comprises airborne end and control you, and described airborne end comprises a range sensor 1, and described range sensor 1 connects a controller 2, and controller 2 connects airborne wireless communication modules 3; Described control you comprises a local wireless communication module 4, and described local wireless communication module 4 connects an early warning controller 5, and early warning controller 5 is connected with early warning module 6.
Due to the main distance of surveying the place ahead barrier, so in the present embodiment, described range sensor is located at front fuselage.
In order to realize multiple alerting pattern, be used in combination, in the present embodiment, described early warning module comprises acousto-optic warning unit.
In the present embodiment, described early warning module is involving vibrations Tip element also.
In the present embodiment, described acousto-optic hint unit comprises pilot lamp and loudspeaker.
In the present embodiment, described pilot lamp is LED light.
For different risk distances are distinguished to early warning, in the present embodiment, described LED light comprises the blue tri-colour LED of reddish yellow.
In the present embodiment, described vibration prompt unit is a vibrating motor.
In the present embodiment, described airborne wireless communication module 3 is 3G communication module.
In the present embodiment, described local wireless communication module 4 is 3G communication module.
The foregoing is only the preferred embodiments of the present invention; not thereby limit the scope of the claims of the present invention; every equivalent structure or conversion of equivalent flow process that utilizes instructions of the present invention and accompanying drawing content to do; or be directly or indirectly used in other relevant technical fields, be all in like manner included in scope of patent protection of the present invention.
Claims (10)
1. unmanned plane obstruction warning system, is characterized in that: comprise airborne end and control you, described airborne end comprises a range sensor, and described range sensor connects a controller, and controller connects an airborne wireless communication module; Described control you comprises a local wireless communication module, and described local wireless communication module connects an early warning controller, and early warning controller is connected with early warning module.
2. unmanned plane obstruction warning system as claimed in claim 1, is characterized in that: described range sensor is located at front fuselage.
3. unmanned plane obstruction warning system as claimed in claim 2, is characterized in that: described early warning module comprises acousto-optic warning unit.
4. unmanned plane obstruction warning system as claimed in claim 3, is characterized in that: described early warning module is involving vibrations Tip element also.
5. unmanned plane obstruction warning system as claimed in claim 4, is characterized in that: described acousto-optic hint unit comprises pilot lamp and loudspeaker.
6. unmanned plane obstruction warning system as claimed in claim 5, is characterized in that: described pilot lamp is LED light.
7. unmanned plane obstruction warning system as claimed in claim 6, is characterized in that: described LED light comprises the blue tri-colour LED of reddish yellow.
8. unmanned plane obstruction warning system as claimed in claim 7, is characterized in that: described vibration prompt unit is a vibrating motor.
9. unmanned plane obstruction warning system as claimed in claim 8, is characterized in that: described airborne wireless communication module is 3G communication module.
10. unmanned plane obstruction warning system as claimed in claim 9, is characterized in that: described local wireless communication module is 3G communication module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310480659.7A CN103531044A (en) | 2013-10-15 | 2013-10-15 | Barrier alarm system for unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201310480659.7A CN103531044A (en) | 2013-10-15 | 2013-10-15 | Barrier alarm system for unmanned aerial vehicle |
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| CN103531044A true CN103531044A (en) | 2014-01-22 |
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| CN201310480659.7A Pending CN103531044A (en) | 2013-10-15 | 2013-10-15 | Barrier alarm system for unmanned aerial vehicle |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104267738A (en) * | 2014-09-25 | 2015-01-07 | 安徽科耀智能科技有限公司 | Anti-collision system for unmanned aerial vehicle |
| CN108053691A (en) * | 2017-12-19 | 2018-05-18 | 广东省航空航天装备技术研究所 | A kind of unmanned plane of unmanned plane anticollision automatic testing method and application this method |
| CN110824127A (en) * | 2019-10-23 | 2020-02-21 | 军事科学院军事医学研究院环境医学与作业医学研究所 | Intelligent unmanned aerial vehicle water quality monitoring cruise operation monitoring and alarm control method |
| CN112325857A (en) * | 2020-10-22 | 2021-02-05 | 中国电子科技集团公司第五十四研究所 | Unmanned aerial vehicle obstacle early warning method based on oblique photography |
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| CN202383293U (en) * | 2011-12-23 | 2012-08-15 | 湖北易瓦特科技有限公司 | Obstacle-anticollision warning system of unmanned helicopter |
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| CN203465855U (en) * | 2013-10-15 | 2014-03-05 | 江苏艾锐泰克无人飞行器科技有限公司 | Obstacle alarm system for unmanned plane |
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Patent Citations (6)
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| CN101807080A (en) * | 2010-03-16 | 2010-08-18 | 浙江大学 | Robot airship control system for overhead line inspection and control method thereof |
| US20120092208A1 (en) * | 2010-10-18 | 2012-04-19 | Lemire Robert A | Systems and methods for collision avoidance in unmanned aerial vehicles |
| CN102529962A (en) * | 2010-12-08 | 2012-07-04 | 安尼株式会社 | Moving body anti-collision device and moving body |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104267738A (en) * | 2014-09-25 | 2015-01-07 | 安徽科耀智能科技有限公司 | Anti-collision system for unmanned aerial vehicle |
| CN108053691A (en) * | 2017-12-19 | 2018-05-18 | 广东省航空航天装备技术研究所 | A kind of unmanned plane of unmanned plane anticollision automatic testing method and application this method |
| CN110824127A (en) * | 2019-10-23 | 2020-02-21 | 军事科学院军事医学研究院环境医学与作业医学研究所 | Intelligent unmanned aerial vehicle water quality monitoring cruise operation monitoring and alarm control method |
| CN112325857A (en) * | 2020-10-22 | 2021-02-05 | 中国电子科技集团公司第五十四研究所 | Unmanned aerial vehicle obstacle early warning method based on oblique photography |
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Application publication date: 20140122 |