A state-dependent control law is proposed using the Lyapunov stability theorem and its usefulness for closed-loop control of a synchronous orbit is investigated. It is shown that a sequential scheme using a modified control law provides a more practical means of orbit control.
Control of Synchronous Orbit Using Lyapunov Stability Theory
IEEE Transactions on Aerospace and Electronic Systems ; AES-17 , 1 ; 48-53
1981-01-01
1499165 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Control of synchronous orbit using Lyapunov stability theory
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