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

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.

authors

• Vadali, Srinivas

published proceedings

• Proceedings of the American Control Conference

author list (cited authors)

• Vadali, S. R.

complete list of authors

• Vadali, SR

publication date

• December 1984

published in

• Proceedings of the ... American Control Conference. American Control Conference  Journal

start page

• 1674

end page

• 1678

volume

• 3