Unmanned aerial vehicle flight control system and method thereof
A flight control system and flight control technology, applied in the direction of control/adjustment system, attitude control, non-electric variable control, etc., can solve the problems of cumbersome procedures, inconvenient use, and high cost
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[0021] It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.
[0022] Implementations of various embodiments of the present invention will now be described with reference to the accompanying drawings. In the following description, use of suffixes such as 'module', 'part' or 'unit' for denoting elements is only for facilitating description of the present invention and has no specific meaning by itself.
[0023] The descriptions involving "first", "second" and so on in the present invention are only for descriptive purposes, and should not be understood as indicating or implying their relative importance or implicitly indicating the number of indicated technical features. Thus, the features defined as "first" and "second" may explicitly or implicitly include at least one of these features. In addition, the technical solutions of the various embodiments can be combined with each ot...
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