Press This book aims at the many disturbance problems existing in the spacecraft attitude control system. based on the linear matrix inequality (LMI) method for multi-objectiv...
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paperback. Condition: New. Paperback.Pub Date:2022-06-01 Pages:384 Language:Chinese Publisher:Science Press This book aims at the many disturbance problems existing in the spacecraft attitude control system. based on the linear matrix inequality (LMI) method for multi-objective optimization of the system Detailed analysis and theoretical research on control problems. The accuracy and stability of spacecraft attitude control are closely related to the terminal small-angle attitude maneuver. and are easily affected by ma. Seller Inventory # NX027908
Quantity: 1 available
Seller: liu xing, Nanjing, JS, China
paperback. Condition: New. Paperback.Pub Date:2022-06-01 Pages:384 Language:Chinese Publisher:Science Press This book aims at the many disturbance problems existing in the spacecraft attitude control system. based on the linear matrix inequality (LMI) method for multi-objective optimization of the system Detailed analysis and theoretical research on control problems. The accuracy and stability of spacecraft attitude control are closely related to the terminal small-angle attitude maneuver. and are easily affected by ma. Seller Inventory # AMZ095275_NX027908_095275
Quantity: 3 available