Title :
Control of Synchronous Orbit Using Lyapunov Stability Theory
Author :
Ahmed, N.U. ; Sen, A.K.
Author_Institution :
University of Ottawa
Abstract :
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.
Keywords :
Acceleration; Councils; Equations; Force control; Lyapunov method; Satellites;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
DOI :
10.1109/TAES.1981.309035
