AbstractThis paper considers the control of entire-formation maneuvering in low-thrust Earth-orbiting spacecraft formation flying (SFF). A coordinated control scheme based on the leader-follower approach is developed to achieve formation maneuvers while keeping the internal formation intact. To implement the control scheme, a low-level sliding mode control (SMC) based on nonlinear dynamics is provided. Using a Lyapunov-based control design and stability analysis technique, we prove that the closed-loop system is globally asymptotically stable. Numerical simulations show the advantage of the controller for fuel cost reductions, tracking accuracy, and effectiveness in ensuring entire-formation maneuvering. An exact nonlinear model with modeled disturbances ( disturbance and bounded uncertainties) is used for dynamic simulation.
Sliding mode control for low-thrust Earth-orbiting spacecraft formation maneuvering
Aerospace Science and Technology ; 10 , 7 ; 636-643
2006-04-19
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
AN ESTIMATOR-BASED SLIDING-MODE CONTROL FOR MANEUVERING A FLEXIBLE SPACECRAFT
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