CN104843193A - Unmanned aerial vehicle lamplight warning system - Google Patents
Unmanned aerial vehicle lamplight warning system Download PDFInfo
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- CN104843193A CN104843193A CN201510241095.0A CN201510241095A CN104843193A CN 104843193 A CN104843193 A CN 104843193A CN 201510241095 A CN201510241095 A CN 201510241095A CN 104843193 A CN104843193 A CN 104843193A
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Abstract
The invention discloses an unmanned aerial vehicle lamplight warning system. The unmanned aerial vehicle lamplight warning system comprises an aerial vehicle body and airfoils fixedly connected with the aerial vehicle body; the aerial vehicle body is internally provided with a controller and a driver; the controller is connected with the driver; the outer surface of the airfoils is embedded with a light emitting diode (LED) lamp; and the LED lamp is connected with the driver. Through multiple LED lamp combinations of different colors or using the blink of the LED lamplight to present different flying states, the unmanned aerial vehicle lamplight warning system is capable of clearly displaying the flying state of the unmanned aerial vehicle to a user, and timely and accurately obtaining the state information of the unmanned aerial vehicle.
Description
Technical field
The present invention relates to unmanned vehicle technical field, is specifically a kind of unmanned vehicle light warning system.
Background technology
At present, the state of flight of unmanned vehicle, mostly by radio transmission, is namely sent to ground based terminal by wireless signal by the communication of unmanned vehicle and ground based terminal.
But still there are some problems in the mode of this transmission over radio:
1, unmanned vehicle state of flight is directly perceived not, also more delayed, controls unmanned vehicle in-flight, sometimes can not notice the state of flight of unmanned vehicle timely, likely can cause the accident user, therefore reliable not.
2, when unmanned vehicle is under the fuzzy environment in insufficient light, the visual field during operation, ground based terminal cannot the information of state of flight of intuitive judgment unmanned vehicle.
Therefore, how to break away from the signal transmission form of single radio transmission, a kind of new device knowing unmanned vehicle state of flight or method and become the target that those skilled in the art pursue.
Summary of the invention
For solving defect in prior art, the invention provides a kind of unmanned vehicle light warning system, reaching the technical purpose being represented unmanned vehicle state by LED.
For achieving the above object, the invention discloses a kind of unmanned vehicle light warning system, comprise aircraft body and the wing affixed with aircraft body, be provided with controller and actuator in aircraft body, controller is connected with actuator; The outside face of wing is embedded with multiple LED, and LED is connected with actuator.
The present invention is combined or multiple flicker fusion by the different colours of LED, and demonstrate the state of flight of unmanned vehicle, live effect is good, can judge the state of flight of unmanned vehicle intuitively.
Further, wing comprises two front wings, two rear wings, each wing is embedded with three LED.
By arranging the mode of LED on each wing, avoiding the problem that LED is blocked by aircraft body when aircraft is in certain deflection angle, ensure that ground handling operator can observe LED all the time.
Further, actuator has two groups of I/O ports, often organizes I/O port and comprises ruddiness I/O port, green glow I/O port and blue light I/O port.
It is red that ruddiness I/O port is used for the display of driving LED lamp, and it is green that green glow I/O port is used for the display of driving LED lamp, and it is blue that blue light I/O port is used for the display of driving LED lamp.The LED that this type of drive more renews when being convenient to or damage aging in LED.
Further, in two groups of I/O ports of actuator, one group is connected with the LED on front wing, and another group is connected with the LED on rear wing
Further, LED is red LED lamp, green light LED lamp or blue LED lamp.
Further, LED is arranged on side or the downside of wing.
The LED of side or downside is more easily observed, and ground handling operator easily obtains the state of flight of aircraft.
Further, the power supply be connected with controller is also comprised.
LED is arranged on side or the downside of wing, is conducive to user and its status information is observed.
Beneficial effect of the present invention is: the state of flight being combined by the LED of multiple different colours or utilized the flicker of LED lamplight to represent different, unmanned vehicle light warning system of the present invention the gem-pure state of flight by unmanned vehicle can be shown to user, can obtain the status information of unmanned vehicle immediately, exactly.
Unmanned vehicle light warning system of the present invention be to existing unmanned vehicle radio communication supplement and perfect, the effect of checking can either be played the information of radio transmission, aircraft flight status information can be known when wireless signal is interfered again.
Accompanying drawing explanation
Fig. 1 is the structural representation of unmanned vehicle light warning system;
Fig. 2 is control structure block diagram of the present invention.
In figure, 1, aircraft body; 2, wing; 3, LED.
Detailed description of the invention
Below in conjunction with accompanying drawing, explanation is explained in detail to structure of the present invention.
The structural representation of unmanned vehicle light warning system as shown in Figure 1, comprise aircraft body 1 and the wing 2 affixed with aircraft body 1, be provided with controller and actuator in aircraft body 1, controller is connected with actuator; The outside face of wing 2 is embedded with multiple LED 3, LED 3 can be arranged on the side of wing 2, also can be arranged on the downside of wing 2, and each LED 3 is connected with actuator respectively, also comprise the power supply be connected with controller, power supply is the light warning system power supply of whole unmanned vehicle.
In the present embodiment, the number of wing 2 is four, comprises two front wings and two rear wings, each wing 2 is embedded with three LED 3, totally ten two LED 3; Actuator in aircraft body 1 has two groups of I/O ports, LED 3 is also divided into two groups, six LED 3 of front wing are one group, six LED 3 of rear wing are one group, the direction of front wing is the direction of head, the direction of rear wing is the direction of tail, often organizes I/O port and comprises ruddiness I/O port, green glow I/O port and blue light I/O port; Often organize I/O port to be connected with the LED 3 on front wing or rear wing, that is two groups of I/O ports of actuator, wherein one group is connected with the LED on front wing, another group is connected with the LED on rear wing, the difference of the driving voltage that each LED 3 can provide according to I/O port or size of current and show different colors.Three LED 3 on each wing 2 are when powering, and can present redness, green, blueness respectively, certainly, the present invention is not limited to specific combination, can set the color of each LED 3 according to actual needs.
As shown in Figure 1, 2, the driving power of all LED 3 is sent by actuator and regulates, and the control signal of actuator is sent by controller.When LED 3 needs display state of flight, controller sends control signal to actuator, and namely actuator lights corresponding LED 3, display real-time flight state.
It should be noted that, " ruddiness I/O port " in the present embodiment is the I/O port driving red light source, and " green glow I/O port " in the present embodiment is the I/O port driving green light source, and " blue light mouth " in the present embodiment is the I/O port driving blue-light source.I/O port of the present invention is I/O port general in circuit.Invention has been the test of the following two kinds situation:
One, when GPS et out of order:
In unmanned vehicle flight course, the navigation information of GPS device Real-time Obtaining unmanned vehicle, GPS device is transferred to controller after obtaining navigation information, controller is understood the statement transmitted, if find that the statement read has problem, or statement cannot be read from GPS device at all, then determine GPS device fault.
Now, controller sends control command to LED 3 actuator, and driver control electric current makes LED 3 light, and in the present embodiment, driver control LED 3 sends the light that reddish yellow replaces quick flashing, breaks down with the GPS device showing unmanned vehicle.
Two, unmanned vehicle makes a return voyage landing situation:
In unmanned vehicle flight course, can automatically to make a return voyage landing, also can to make a return voyage after receiving the control command that ground controller sends landing, if controllers sends on ground instruction of making a return voyage, controller can be transferred to after wireless device then on unmanned vehicle receives, after corresponding statement understood by controller, just control command is sent to actuator, after actuator receives instruction, driving LED lamp 3 is lighted, in the present embodiment, driver control LED 3 sends red light, is in show unmanned vehicle landing state of making a return voyage.Automatically make a return voyage landing in LED 3 light identical with said process.
The foregoing is only preferred embodiment of the present invention, not in order to limit the present invention, all do in flesh and blood of the present invention any amendment, equivalent to replace and simple modifications etc., all should be included within protection scope of the present invention.
Claims (7)
1. a unmanned vehicle light warning system, comprises aircraft body (1) and the wing affixed with aircraft body (2), it is characterized in that: be provided with controller and actuator in aircraft body, controller is connected with actuator; The outside face of wing is embedded with LED (3), and LED is connected with actuator.
2. unmanned vehicle light warning system according to claim 1, is characterized in that: wing comprises two front wings, two rear wings, each wing is embedded with three LED.
3. unmanned vehicle light warning system according to claim 1 and 2, is characterized in that: actuator has two groups of I/O ports, often organizes I/O port and comprises ruddiness I/O port, green glow I/O port and blue light I/O port.
4. unmanned vehicle light warning system according to claim 3, is characterized in that: in two groups of I/O ports of actuator, one group is connected with the LED on front wing, and another group is connected with the LED on rear wing.
5. unmanned vehicle light warning system according to claim 1, is characterized in that: LED is red LED lamp, green light LED lamp or blue LED lamp.
6. unmanned vehicle light warning system according to claim 1, is characterized in that: LED is arranged on side or the downside of wing.
7. unmanned vehicle light warning system according to claim 1, is characterized in that: also comprise the power supply be connected with controller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201510241095.0A CN104843193A (en) | 2015-05-13 | 2015-05-13 | Unmanned aerial vehicle lamplight warning system |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201510241095.0A CN104843193A (en) | 2015-05-13 | 2015-05-13 | Unmanned aerial vehicle lamplight warning system |
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| CN104843193A true CN104843193A (en) | 2015-08-19 |
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| CN201510241095.0A Pending CN104843193A (en) | 2015-05-13 | 2015-05-13 | Unmanned aerial vehicle lamplight warning system |
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Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105629991A (en) * | 2016-01-29 | 2016-06-01 | 谭圆圆 | Flying prompt device and method for unmanned aerial vehicle |
| CN105711848A (en) * | 2016-02-22 | 2016-06-29 | 苏州黄章妹族工业设计有限公司 | Unmanned aerial vehicle with alarm function |
| CN105913634A (en) * | 2016-04-18 | 2016-08-31 | 王竹林 | An unmanned aerial vehicle safety control system, a method, an unmanned aerial vehicle and a remote controller |
| CN106005411A (en) * | 2016-07-14 | 2016-10-12 | 辽宁猎鹰航空科技有限公司 | Intelligent warning system for unmanned aerial vehicle |
| CN106143935A (en) * | 2016-07-26 | 2016-11-23 | 广东容祺智能科技有限公司 | A kind of highly compatible low electricity warning unmanned plane pilot indicating lamp and indicating means |
| CN107074377A (en) * | 2016-12-29 | 2017-08-18 | 深圳市大疆创新科技有限公司 | A kind of control method, device, equipment and unmanned plane |
| CN107085433A (en) * | 2016-02-16 | 2017-08-22 | 松下电器（美国）知识产权公司 | Emission control device, unmanned vehicle and light-emitting control method |
| CN107203218A (en) * | 2016-03-16 | 2017-09-26 | 零度智控（北京）智能科技有限公司 | Make a return voyage line-hunting method, device and aircraft |
| CN108153327A (en) * | 2017-12-07 | 2018-06-12 | 浙江大学 | Formation light show system and control method outside a kind of quadrotor room |
| CN108571964A (en) * | 2018-06-08 | 2018-09-25 | 赫星科技有限公司 | Unmanned plane positioning navigation device and its control method |
| FR3080094A1 (en) * | 2018-04-16 | 2019-10-18 | Airbus Helicopters | METHOD FOR PREPARING TO TAKE OFF A DRONE, DRONE AND PREPARATION SYSTEM THEREOF |
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| CN201244361Y (en) * | 2008-07-16 | 2009-05-27 | 胡伟强 | Remotely-controlled aircraft with airfoil lamp |
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Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN105629991A (en) * | 2016-01-29 | 2016-06-01 | 谭圆圆 | Flying prompt device and method for unmanned aerial vehicle |
| CN107085433A (en) * | 2016-02-16 | 2017-08-22 | 松下电器（美国）知识产权公司 | Emission control device, unmanned vehicle and light-emitting control method |
| CN107085433B (en) * | 2016-02-16 | 2021-08-10 | 松下电器（美国）知识产权公司 | Light emission control device, unmanned aerial vehicle, and light emission control method |
| CN105711848A (en) * | 2016-02-22 | 2016-06-29 | 苏州黄章妹族工业设计有限公司 | Unmanned aerial vehicle with alarm function |
| CN107203218B (en) * | 2016-03-16 | 2020-01-07 | 天津远翥科技有限公司 | Return route line seeking method and device and aircraft |
| CN107203218A (en) * | 2016-03-16 | 2017-09-26 | 零度智控（北京）智能科技有限公司 | Make a return voyage line-hunting method, device and aircraft |
| CN105913634A (en) * | 2016-04-18 | 2016-08-31 | 王竹林 | An unmanned aerial vehicle safety control system, a method, an unmanned aerial vehicle and a remote controller |
| CN105913634B (en) * | 2016-04-18 | 2019-06-21 | 王竹林 | Unmanned vehicle safety control system, method, unmanned vehicle and remote controler |
| CN106005411A (en) * | 2016-07-14 | 2016-10-12 | 辽宁猎鹰航空科技有限公司 | Intelligent warning system for unmanned aerial vehicle |
| CN106143935A (en) * | 2016-07-26 | 2016-11-23 | 广东容祺智能科技有限公司 | A kind of highly compatible low electricity warning unmanned plane pilot indicating lamp and indicating means |
| CN107074377A (en) * | 2016-12-29 | 2017-08-18 | 深圳市大疆创新科技有限公司 | A kind of control method, device, equipment and unmanned plane |
| CN107074377B (en) * | 2016-12-29 | 2019-06-25 | 深圳市大疆创新科技有限公司 | A kind of control method, device, equipment and unmanned plane |
| CN108153327A (en) * | 2017-12-07 | 2018-06-12 | 浙江大学 | Formation light show system and control method outside a kind of quadrotor room |
| CN108153327B (en) * | 2017-12-07 | 2020-05-19 | 浙江大学 | Four-rotor aircraft outdoor formation light performance system and control method |
| FR3080094A1 (en) * | 2018-04-16 | 2019-10-18 | Airbus Helicopters | METHOD FOR PREPARING TO TAKE OFF A DRONE, DRONE AND PREPARATION SYSTEM THEREOF |
| US11511849B2 (en) | 2018-04-16 | 2022-11-29 | Airbus Helicopters | Method of preparing a drone for takeoff, and an associated drone and preparation system |
| CN108571964A (en) * | 2018-06-08 | 2018-09-25 | 赫星科技有限公司 | Unmanned plane positioning navigation device and its control method |
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Effective date of registration: 20180223 Address after: No. 309-9, service center, Chen Tong, Hexi District, Dongting Road, Hexi District, Tianjin, Tianjin Applicant after: Tianjin far Zhu Technology Co. Ltd. Address before: 100094 Beijing, Haidian District, northeast Wang West Road, No. 8 Zhongguancun Software Park, building 9, 203 Applicant before: Zero degree intelligence control (Beijing) intelligent Science and Technology Ltd. |
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Application publication date: 20150819 |
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