Finite time control method for quadrotor aircraft based on hyperbolic tangent enhanced constant-speed approach law and fast terminal sliding mode surface
A quadrotor aircraft, hyperbolic tangent technology, applied in non-electric variable control, control/regulation systems, three-dimensional position/channel control, etc. Reaching the sliding surface and approaching speed and other issues
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[0073] The present invention will be further described below in conjunction with the accompanying drawings.
[0074] refer to Figure 1-Figure 7 , a finite-time control method for quadrotor aircraft based on hyperbolic tangent-enhanced constant-velocity reaching law and fast terminal sliding surface, including the following steps:
[0075] Step 1, determine the transfer matrix from the body coordinate system based on the quadrotor aircraft to the inertial coordinate system based on the earth;
[0076]
[0077] Among them, ψ, θ, and φ are the yaw angle, pitch angle, and roll angle of the aircraft, respectively, indicating the rotation angle of the aircraft around each axis of the inertial coordinate system in turn, and T ψ represents the transition matrix of ψ, T θ Denotes the transition matrix of θ, T φ Represents the transition matrix of φ;
[0078] Step 2, analyze the quadrotor aircraft dynamics model according to the Newton Euler formula, the process is as follows: ...
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