Nonsingular terminal sliding mode flight path control method for airships
A non-singular terminal, control method technology, applied in the field of automatic control, can solve problems such as convergence
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[0095] With reference to accompanying drawing, a kind of airship non-singular terminal sliding mode track control method of the present invention is introduced in detail, and its specific steps are as follows:
[0096] Step 1: Given command track
[0097] The given command track is:
[0098] n d =[x d ,y d ,z d ,θ d ,ψ d ,φ d ] T =[(1.5t)m,200sin(0.005t)m,10m,0rad,0.02rad,0rad] T , x d 、y d ,z d , θ d 、ψ d and φ d They are command x coordinate, command y coordinate, command z coordinate, command pitch angle, command yaw angle and command roll angle;
[0099] Step 2: Calculate the amount of error
[0100] Calculate the amount of error between the commanded track and the actual track:
[0101] e=η-η d =[x-x d ,y-y d ,z-z d ,θ-θ d ,ψ-ψ d ,φ-φ d ] T ,
[0102] where, η=[x,y,z,θ,ψ,φ] T is the actual track, x, y, z, θ, ψ, φ are the x coordinate, y coordinate, z coordinate, pitch angle, yaw angle and roll angle of the actual track respectively, which are co...
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