This invention discloses a dual non-fragile control method for non-cooperative
spacecraft based on electromagnetic capture, comprising: S1, establishing a dynamic model of the
relative motion of the non-cooperative
spacecraft under electromagnetic capture based on the T-H equations; S2, considering comprehensive disturbances and
rewriting the dynamic model into state-space form; S3, designing a dual non-fragile observer / controller to address the coexistence of additive / multiplicative
gain perturbations in the observer and controller; S4, substituting the dual non-fragile observer / controller into the state-space equations in step S2 to establish a state-
space model of the closed-loop electromagnetic capture
system; S5, deriving sufficient conditions for the
system to be uniformly eventually bounded based on the LMI method and
Lyapunov stability theorem, and solving for the observer / controller parameters in step S3. This invention fully considers the complex situation of coexistence of additive / multiplicative
gain perturbations in the observer and controller, and can solve the electromagnetic capture control problem of non-cooperative
spacecraft under multi-source disturbances such as external interference, elliptical
orbit eccentricity, and unknown
mass.