Control method of quadrotor aircraft based on improved mpc-pid
A technology of a quadrotor aircraft and a control method, applied in attitude control, control/adjustment system, non-electric variable control, etc., can solve problems such as poor dynamic performance, achieve fast response speed and dynamic performance, reduce the amount of calculation and controller The effect of design sophistication
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[0079] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
[0080] Such as figure 1 and figure 2 As shown, a quadrotor aircraft control method based on improved MPC-PID, the specific steps are as follows:
[0081] S1. Establish a dynamic model of the quadrotor aircraft based on the structure and mechanics of the quadrotor aircraft.
[0082] Assume that the quadrotor aircraft is a rigid body, ignoring the vibration and elastic deformation of the body; the structure of the quadrotor aircraft is completely symmetrical,...
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