A tail adjustment mechanism capable of independent pitch and yaw adjustment and an orthopter
A technology of adjusting mechanism and empennage, which is applied in the field of flapping aircraft, can solve the problems of reducing control precision, achieve the effects of improving control precision, avoiding mutual interference, and reducing control difficulty
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[0037] The idea, specific structure and technical effects of the present invention will be clearly and completely described below in conjunction with the embodiments and accompanying drawings, so as to fully understand the purpose, scheme and effect of the present invention. It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other.
[0038] It should be noted that, unless otherwise specified, when a feature is called "fixed" or "connected" to another feature, it can be directly fixed and connected to another feature, or indirectly fixed and connected to another feature. on a feature. In addition, descriptions such as up, down, left, and right used in the present invention are only relative to the mutual positional relationship of the components of the present invention in the drawings.
[0039] Also, unless defined otherwise, all technical and scientific terms used herei...
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