FEEDBACK CONTROL OF FLEXIBLE SPACECRAFT LARGE-ANGLE MANEUVERS USING LIAPUNOV THEORY. Conference Paper uri icon

abstract

  • Feedback control laws are obtained for large-angle maneuvers of flexible spacaecraft using Lyapunov stability theory. The closed-loop distributed parameter system is shown to be stable. Simulation of the closed-loop system is performed by discretization using the assumed modes method.

author list (cited authors)

  • Vadali, S. R.

publication date

  • December 1984