A key technology for visual guidance of an unmanned helicopter
A technology for helicopters and visual guidance, applied in the field of visual guidance, can solve the problems of inability to guarantee safety, easy interference of electromagnetic signals, and inability to guarantee full coverage of guidance.
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[0004] The present invention is implemented as follows, visual guidance process and transformation of the coordinate system, the parameters that can be obtained by the airborne equipment that can be used in the visual guidance process-the aircraft altitude obtained by the altimeter, the attitude angle of the aircraft obtained by the gyroscope, and the gimbal The attitude angle of the camera relative to the aircraft and the focal length obtained by the focus measuring equipment are determined, and how these parameters are used to simplify the pose estimation of the unmanned helicopter; The two stages are introduced, and on this basis, the different guidance methods of the two stages are determined; the theoretical basis of the visual guidance process, various coordinate systems and the conversion relationship in application.
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