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Aircraft mobile landing system and mobile landing method

A technology of aircraft and landing platform, which is applied in the field of aircraft, and can solve the problems of increased difficulty in landing of multi-axis aircraft, shaking of multi-axis aircraft fuselage, accidental damage of aircraft, etc.

Active Publication Date: 2017-03-15
ZHUHAI PANSHI ELECTRONICS TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Usually, computer vision uses color or shape to distinguish and identify objects. It is common to use infrared light sources as identification targets. However, under sunlight, it is susceptible to interference from ambient infrared rays, which leads to interference from multiple identification objects when computer vision identifies targets.
Furthermore, when the multicopter is close to the landing target, due to airflow disturbance or external interference, etc., the fuselage of the multicopter may shake, which in turn causes the camera to shake, and it is difficult for the computer vision system to identify and align the shaking landing target image. making it impossible to land stably on the landing platform
Further, when the landing target is on the moving landing platform, the landing target itself is also shaking, thus further increasing the landing difficulty of the multicopter, which may cause accidental damage to the aircraft

Method used

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  • Aircraft mobile landing system and mobile landing method

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Embodiment Construction

[0024] like figure 1 As shown, the aircraft 1 below is provided with a camera 10, and the camera 10 can include a camera 11 with the lens facing down as the first camera, a camera 12 as the second camera with the lens facing the front and bottom, and a camera 12 as the second camera with the lens facing the rear and the bottom. The camera 13 of the camera, preferably, the three cameras are linearly arranged and located in the same vertical plane, and each camera is provided with a filter, wherein the filter is set to transmit light of a predetermined wavelength, such as infrared rays, etc. . When the aircraft 1 is flying straight ahead, the camera 12 can face forward and downward while the camera 13 can face rear and downward. The angle between the camera 12 and the camera 11, the angle between the camera 13 and the camera 11 are preferably set to be equal, the angle can be selected in the range of 0 to 90 degrees, further preferably, the angle can be Choose from the range o...

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Abstract

The invention provides an aircraft mobile landing system and an aircraft mobile landing method using the system; the aircraft mobile landing system comprises a camera arranged on the aircraft and a landing target arranged on a landing platform; the landing target is provided with a light source sending lights with the preset wavelength; a controller controls the light source to flash according to a preset frequency; the camera comprises a filter sheet allowing the light with the preset wavelength to pass; the landing platform is provided with a first communication module; the aircraft is provided with a second communication module communicating with the first communication module; the system and method allow the aircraft to stably land in mobile, and the landing process has small external interferences.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a mobile landing system and a mobile landing method for multi-axis aircraft. Background technique [0002] At present, aircrafts such as multicopters usually land automatically through computer vision systems, use cameras to obtain images of landing targets, identify and align landing targets through computer vision, and land safely on landing platforms. Usually, computer vision uses color or shape to distinguish and identify objects. It is common to use infrared light sources as identification targets. However, under sunlight, it is susceptible to interference from ambient infrared rays, causing computer vision to be interfered by multiple identification objects when identifying targets. Furthermore, when the multicopter is close to the landing target, due to airflow disturbance or external interference, etc., the fuselage of the multicopter may shake, which in turn causes the ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D45/08H04N7/18
CPCH04N7/181B64D45/08G05D1/0684
Inventor 何春旺
Owner ZHUHAI PANSHI ELECTRONICS TECH CO LTD
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