Pose control distribution method of aircraft based on multiple execution mechanisms
A multi-actuator and attitude control technology, which is applied in the field of attitude control distribution of aircraft, can solve the problem of idealization of assumed conditions and achieve the effect of improving fault tolerance
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[0060] In order to illustrate the present invention more clearly, the present invention will be further described below in conjunction with preferred embodiments and accompanying drawings. Similar parts in the figures are denoted by the same reference numerals. Those skilled in the art should understand that the content specifically described below is illustrative rather than restrictive, and should not limit the protection scope of the present invention.
[0061] Such as figure 1 As shown, the attitude control distribution method based on the multi-actuator aircraft (hereinafter referred to as the aircraft) provided by the present embodiment includes the following steps:
[0062] S1, establish the attitude kinematics equation of the aircraft;
[0063] S2. Determine the attitude angle of the aircraft through the attitude transformation matrix;
[0064] S3, establishing the attitude dynamic equation of the aircraft;
[0065] S4. Calculate the desired control moment of the a...
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