Steady flight control method of multi-rotor unmanned aerial vehicle
A multi-rotor unmanned, flight control technology, applied in attitude control, non-electric variable control, control/regulation systems, etc., can solve problems such as difficult to achieve complex tasks
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[0019] The present invention will be further described below in conjunction with the accompanying drawings.
[0020] figure 1 For the design flowchart of the present invention, the design of the aircraft neural network controller can be completed by the illustrated steps:
[0021] A stable flight control method for a multi-rotor unmanned aerial vehicle, comprising the steps of:
[0022] 1) Obtain the real-time flight data of the aircraft itself through the onboard attitude sensor and the corresponding height and position sensors on the multi-rotor UAV, establish the dynamic model of the aircraft, and use the processor on the multi-rotor UAV to control the aircraft Carry out corresponding analytical processing for the kinematics problem;
[0023] 2) According to the variable parameter convergence differential neural dynamics design method, design a variable parameter convergence differential neural network solver for the multi-rotor aircraft dynamics model;
[0024] 3) Utili...
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