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Volumn 41, Issue 2, 1997, Pages 121-130
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Design of a reduced order H∞ robust controller for an expendable launch vehicle in the presence of structured and unstructured parameter uncertainty
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Author keywords
[No Author keywords available]
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Indexed keywords
BENDING (DEFORMATION);
COMPUTER SIMULATION;
CONTROL SYSTEM ANALYSIS;
CONTROL SYSTEM SYNTHESIS;
FUEL SLOSHING;
MATHEMATICAL MODELS;
OPTIMAL CONTROL SYSTEMS;
PARAMETER ESTIMATION;
ROBUSTNESS (CONTROL SYSTEMS);
STATE SPACE METHODS;
SYSTEM STABILITY;
THREE TERM CONTROL SYSTEMS;
BALANCED TRUNCATION;
EXPENDABLE LAUNCH VEHICLES;
STATE SPACE TRUNCATION;
UNSTRUCTURED PARAMETER UNCERTAINTY;
ROCKET ENGINES;
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EID: 0031177657
PISSN: 00945765
EISSN: None
Source Type: Journal
DOI: 10.1016/S0094-5765(97)00191-4 Document Type: Article |
Times cited : (9)
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References (10)
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