Multi-rotor craft control allocation method
A technology for multi-rotor aircraft and control distribution, which is applied in the field of flight control of multi-rotor aircraft, can solve the problems of undisclosed multi-rotor aircraft control distribution methods, etc., and achieve the effects of improving control distribution efficiency, easy implementation, and simple principle
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[0031] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be clear that the specific embodiments described here are only used to explain the present invention, but not to limit the present invention.
[0032] The invention provides a control distribution method for a multi-rotor aircraft, the principle structure of which is as follows figure 1 shown. The expected attitude angle and altitude calculation module calculates the expected attitude angle and altitude value according to the corresponding attitude angle and altitude commands, and subtracts the actual attitude angle and altitude value of the multi-rotor aircraft fed back by the attitude angle and altitude sensor to obtain the attitude Angle and altitude control errors. The control quantity calculation module obtains the corresponding pitc...
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