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H ∞　Optimal Controller Design and Reduction for the Inertial Hold Mode of the Attitude Control System of the XTE Spacecraft

Author(s):
Publication title:
NASA Technical Reports
Pub. Year:
1994
Issue:
NASA-CR-195137
No.:
G3/37 0205068
Pt.:
NAS 1.26:195137
Paper no.:
N94-24846
Page(from):
1
Page(to):
27
Pages:
27
Pub. info.:
National Aeronautics and Space Adminstration
Language:
English
Type:
Technical Paper

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