CN203465855U - Obstacle alarm system for unmanned plane - Google Patents
Obstacle alarm system for unmanned plane Download PDFInfo
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- CN203465855U CN203465855U CN201320634776.XU CN201320634776U CN203465855U CN 203465855 U CN203465855 U CN 203465855U CN 201320634776 U CN201320634776 U CN 201320634776U CN 203465855 U CN203465855 U CN 203465855U
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- unmanned plane
- communication module
- wireless communication
- warning system
- controller
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Abstract
The utility model relates to a flying control system for an unmanned plane and particularly relates to an obstacle alarm system for the unmanned plane. The system includes an airborne end and a console end. The airborne end includes a distance sensor. The distance sensor is connected with a controller. The controller is connected with an airborne wireless communication module. The console end includes a local wireless communication module which is connected with an early-warning controller. The early-warning controller is connected with an early-warning prompt module. In a flying process, the distance sensor of the obstacle alarm system for the unmanned plane monitors whether there is any obstacle ahead; when an obstacle exists, early-warning information is sent to the console end through the airborne wireless communication module; the console end carries out early-warning prompting after receiving signals so that operation personnel are capable of adjusting the flying state of the unmanned plane so as to prevent loss which is caused when the unmanned plane collides with the obstacle.
Description
Technical field
The utility model 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 utility model provides a kind of can carry out obstruction forewarning to operating personnel, prevent the unmanned plane obstruction warning system of maloperation.
To achieve these goals, the utility model 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 utility model 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 utility model embodiment;
Fig. 2 is the control you modular structure schematic diagram of the utility model embodiment.
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 preferred embodiment of the present utility model; not thereby limit the scope of the claims of the present utility model; every equivalent structure or conversion of equivalent flow process that utilizes the utility model instructions 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 utility model.
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 |
|---|---|---|---|
| CN201320634776.XU CN203465855U (en) | 2013-10-15 | 2013-10-15 | Obstacle alarm system for unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320634776.XU CN203465855U (en) | 2013-10-15 | 2013-10-15 | Obstacle alarm system for unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203465855U true CN203465855U (en) | 2014-03-05 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320634776.XU Expired - Fee Related CN203465855U (en) | 2013-10-15 | 2013-10-15 | Obstacle alarm system for unmanned plane |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103531044A (en) * | 2013-10-15 | 2014-01-22 | 江苏艾锐泰克无人飞行器科技有限公司 | Barrier alarm system for unmanned aerial vehicle |
| 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 |
| CN104269078A (en) * | 2014-09-23 | 2015-01-07 | 苏州天益航空科技有限公司 | Method for collision detection for agricultural plant protection unmanned aerial vehicle |
-
2013
- 2013-10-15 CN CN201320634776.XU patent/CN203465855U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103531044A (en) * | 2013-10-15 | 2014-01-22 | 江苏艾锐泰克无人飞行器科技有限公司 | Barrier alarm system for unmanned aerial vehicle |
| CN104269078A (en) * | 2014-09-23 | 2015-01-07 | 苏州天益航空科技有限公司 | Method for collision detection for agricultural plant protection unmanned aerial vehicle |
| 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 |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140305 Termination date: 20141015 |
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| EXPY | Termination of patent right or utility model |