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Lighting method and device of aircraft and aircraft

A lighting method and technology for an aircraft, applied in the field of aircraft lighting, can solve the problems of poor lighting effect, energy waste, and poor obstacle avoidance effect of the aircraft lighting system, and achieve the effects of solving the poor lighting effect, avoiding energy waste, and improving utilization rate

Active Publication Date: 2021-07-02
SUZHOU EAVISION ROBOTIC TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The object of the present invention is to disclose an aircraft lighting method, device and aircraft to solve the problem of poor lighting effect and energy waste in the aircraft lighting system in the prior art And lead to the problem of poor obstacle avoidance effect

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  • Lighting method and device of aircraft and aircraft
  • Lighting method and device of aircraft and aircraft
  • Lighting method and device of aircraft and aircraft

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Embodiment Construction

[0054] The present invention will be described in detail below in conjunction with the implementations shown in the drawings, but it should be noted that these implementations are not limitations of the present invention, and those of ordinary skill in the art based on the functions, methods, or structural changes made by these implementations Equivalent transformations or substitutions all fall within the protection scope of the present invention.

[0055] Such as figure 1 As shown, this embodiment provides an aircraft, which includes: a flight control system 100, used to obtain the light-spotting area M of the lighting system and obstacle parameters; a lighting system 200 connected to the flight control system 100, used to obtain the lighting system The luminous intensity L per unit area of ​​200 and the preset range of spotlight distance (the preset range of spotlight distance can be configured as the preset value set by the internal system of the aircraft, or a user-define...

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Abstract

The invention provides a lighting method and device of an aircraft and the aircraft. The lighting method of the aircraft comprises the steps of obtaining the unit area luminous intensity, the condensation area and the condensation distance preset range of a lighting system, and determining a target condensation distance and a target condensation angle of the lighting system; acquiring obstacle parameters, and determining the current condensation distance of the lighting system based on the relationship between the obstacle parameters and the target condensation distance; and adjusting the target condensation angle based on the current condensation distance so as to control the lighting system to perform lighting according to the unit area luminous intensity, the condensation area and the adjusted condensation angle. The problems that an aircraft lighting system in the prior art is poor in lighting effect, energy is wasted, and the obstacle avoidance effect is poor are solved.

Description

technical field [0001] The invention relates to the technical field of aircraft lighting, in particular to an aircraft lighting method, device and aircraft. Background technique [0002] UAV is an unmanned UAV operated by wireless remote control equipment or its own program control device. At present, in the civilian field, map surveying UAVs, geological survey UAVs, disaster monitoring UAVs, weather detection UAVs, air traffic control UAVs, border control UAVs, communication relay UAVs The research and application of drones, pesticide spraying drones, etc. are constantly developing at home and abroad. [0003] The existing LEDs for drone lighting are used to provide lighting for the sensors on the drone, such as the visual sensor for the user to detect obstacles. While adjusting the focusing distance of the drone, the lighting area is generally increased at the same time. , if the illumination brightness is kept constant, the lighting power of the UAV will increase, which...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/12B64D47/04F21V7/00F21V14/04H05B47/115G03B15/02F21W107/30
CPCG05D1/12F21V7/00F21V14/04H05B47/115G03B15/02B64D47/04F21W2107/30Y02B20/40
Inventor 王新宇宋红军董雪松
Owner SUZHOU EAVISION ROBOTIC TECH CO LTD
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