This paper considers the problem of relative motion control for spacecraft formation flying (SFF). Using terminal sliding mode technique, a relative position/velocity tracking control based on the nonlinear model is developed. The presented controller enables rapid formation reconfiguration with feasible fuel cost and strong robustness in the presence of uncertain but bounded disturbances. A nonlinear model with J2 disturbance and bounded uncertainties is used for dynamic simulation.
Terminal Sliding Mode Control for Spacecraft Formation Flying
IEEE Transactions on Aerospace and Electronic Systems ; 45 , 3 ; 835-846
2009-07-01
3086744 byte
Article (Journal)
Electronic Resource
English
Terminal Sliding Mode Control for Spacecraft Formation Flying
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