Vision auxiliary device and method for automatic landing of unmanned aerial vehicle

An auxiliary device and unmanned aerial vehicle technology, applied in the field of unmanned aerial vehicles, can solve the problems of difficulty in meeting landing requirements, poor attitude and position calibration effect, lack of multi-scale analysis mechanism, etc., and achieves low power consumption, simple structure, and processing speed. quick effect

Inactive Publication Date: 2015-07-29
CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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AI Technical Summary

Problems solved by technology

[0004] In order to solve the lack of multi-scale analysis mechanism in the existing visual aid devices that use airborne camera equipment to obtain and identify the runway and horizon to perceive the landing attitude of the UAV, it is difficult to meet the landing requirem

Method used

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  • Vision auxiliary device and method for automatic landing of unmanned aerial vehicle
  • Vision auxiliary device and method for automatic landing of unmanned aerial vehicle
  • Vision auxiliary device and method for automatic landing of unmanned aerial vehicle

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[0038] The present invention will be further described in detail below in conjunction with the drawings.

[0039] Such as figure 1 As shown, the visual aid device for autonomous landing of the UAV of the present invention is mainly composed of a two-axis turntable, a turntable motor, a power supply module, a monocular fixed focus camera, a visual aid information processing module and an information storage module. The two-axis turntable is installed at the head of the drone. The turntable motor, power supply module, monocular fixed focus camera, visual auxiliary information processing module and information storage module are all fixed on the two-axis turntable; the turntable motor is connected to the two-axis turntable. It drives the two-axis turntable to move; the power module is connected to the turntable motor, monocular fixed focus camera, visual auxiliary information processing module and information storage module, and is used to feed the turntable motor, monocular fixed fo...

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Abstract

The invention discloses a vision auxiliary device and method for automatic landing of an unmanned aerial vehicle, and relates to the field of unmanned aerial vehicles. The problems that according to an existing vision auxiliary device which acquires and recognizes runways and the horizon through an airborne photographing device so as to sense the landing posture of the unmanned aerial vehicle, due to the lack of a multi-scale analysis mechanism, the landing requirement cannot be easily met, the posture and position calibration effect is poor, and deep prediction of the movement behavior of the unmanned aerial vehicle lacks are solved. The vision auxiliary device comprises a two-shaft rotary table, a rotary table motor, a power module, a single-view fixed-focus camera, a vision auxiliary information processing module and an information storage module. The vision auxiliary information processing module comprises a landing track re-planning module, a data comparator, an information filter, a computer vision processor based on image control, a computer vision processor based on position control, a first feedback correction device, a second feedback correction device, an information fusion parameter extractor and an RS485 communication interface. The vision auxiliary device is simple in structure, low in power consumption, high in efficiency and good in compatibility.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a visual aid device and a visual aid method for autonomous landing of unmanned aerial vehicles. Background technique [0002] Acquisition and cooperative control of UAV position and attitude information are the core of UAV autonomous landing technology. In the landing area, adjust the pitch attitude and heading offset; after sensing the approach (the process of aligning the aircraft with the runway when it descends), obtain the position and attitude information of the UAV in real time, and align the heading with the UAV flight control system, according to the plan When planning the leveling point, ensure that the flight parameters of the drone meet the landing conditions, and turn off the engine to land according to the leveling track line; finally, during the taxiing and braking phase, ensure that the drone can slide along the airport runway line to avoid Exit ...

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Application Information

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IPC IPC(8): G05D1/10
Inventor 江晟贾宏光厉明马经纬李银海
Owner CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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