DocumentCode :
300838
Title :
Stability of the nonlinear motions of a satellite
Author :
Chattergy, Rahul
Author_Institution :
Hawaii Univ., Honolulu, HI, USA
Volume :
5
fYear :
1995
fDate :
21-23 Jun 1995
Firstpage :
3620
Abstract :
The libration of an extensible dumbbell satellite in a circular Earth orbit is given by a pair of nonlinear second-order ordinary differential equations. Stability of the paths about the origin of the phase space is analyzed by Lyapunov´s indirect method. It is also shown that ad hoc assumptions commonly used to transform the nonlinear equations into linear equations do not produce reliable stability criterion for libration
Keywords :
Lyapunov methods; aerospace control; artificial satellites; motion control; nonlinear differential equations; phase space methods; stability; Lyapunov indirect method; artificial satellite; circular Earth orbit; extensible dumbbell satellite; libration; nonlinear motions; nonlinear second-order differential equations; phase space; stability; Ear; Earth; Nonlinear equations; Nonlinear systems; Satellites; Springs; Stability analysis; Stability criteria; Steady-state; Transforms;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, Proceedings of the 1995
Conference_Location :
Seattle, WA
Print_ISBN :
0-7803-2445-5
Type :
conf
DOI :
10.1109/ACC.1995.533812
Filename :
533812
Link To Document :
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