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      An approach to structure/control simultaneous optimization for largeflexible spacecraft

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      AIAA Journal
      American Institute of Aeronautics and Astronautics (AIAA)

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          Optimal simultaneous structural and control design of maneuvering flexible spacecraft

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            Eigenvalue optimization algorithms for structure/controller design iterations

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              Enhanced vibration controllability by minor structural modifications

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                Author and article information

                Journal
                AIAA Journal
                AIAA Journal
                American Institute of Aeronautics and Astronautics (AIAA)
                0001-1452
                1533-385X
                August 1987
                August 1987
                : 25
                : 8
                : 1133-1138
                Article
                10.2514/3.9754
                fe9faeef-1ae1-4809-a3a4-d18f1d06d9c2
                © 1987
                History

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