A landing gear control method and device for an unmanned aerial vehicle
A technology of unmanned aerial vehicle and control method, which is applied to the chassis and other directions, can solve the problems of loss of tripod support, low accuracy, poor safety, etc., and achieve the effect of avoiding damage
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[0018] Certain terms are used throughout the description and claims to refer to particular components. It should be understood by those skilled in the art that manufacturers may use different terms to refer to the same component. The specification and claims do not use the difference in name as a way to distinguish components, but use the difference in function of components as a basis for distinction. The present invention will be described in detail below in conjunction with the accompanying drawings and embodiments.
[0019] figure 1 It is a structural schematic diagram of the landing gear control device of the unmanned aerial vehicle according to the embodiment of the present invention. Such as figure 1 As shown, the device includes: a status acquisition module 10 , an instruction acquisition module 20 , a first judging module 30 , a second judging module 40 and a control module 50 .
[0020] The state acquiring module 10 is used to acquire the current state of the UAV...
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