An Anti-jamming Controller for Mars Lander under Unknown Frequency Harmonic Interference
A harmonic interference and lander technology, applied in attitude control, aerospace aircraft, aircraft and other directions, can solve the problems of inability to estimate and eliminate interference, poor adaptability, energy loss, etc., to enhance engineering application value and improve adaptability performance and anti-interference
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[0069] Such as figure 1 Shown, the specific implementation steps of the present invention are as follows (below taking the Mars lander control system as an example to illustrate the specific realization of the method):
[0070] 1. Build the attitude kinematics and dynamics model of the Mars lander
[0071] The attitude kinematics and dynamics model of the Mars lander under the condition of unknown frequency harmonic interference is built as follows:
[0072]
[0073]
[0074]
[0075] in,
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[0077] J is the moment of inertia matrix of the lander and is taken as J 12 =J 13 =J 12 =J 23 =J 13 =J 23 =0,J 11 =963kg·m 2 , J 22 =1170kg·m 2 , J 33 =1382kg·m 2 , ω=[ω x ,ω y ,ω z ] T is the triaxial angular velocity ω 0 =[0.1,0.1,0.1] T rad / s, ω d =[0.01sin(πt / 75),0.02sin(πt / 75),-0.01sin(πt / 75)] T , σ=[σ x ,σ y ,σ z ] T is the triaxial Rodrigue parameter σ 0 =[-1,-1,1] T , σ d =[0.1,0.15,0.2] T , u=[u x ,u y ,u z ] T Represents three-...
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