Work during this period was concerned with: 1) development of a new method for the derivation of the state equations of motion for the control of flexible spacecraft in terms of quasi-coordinates; and 2) development of a method for the control of spacecraft in the form of articulated flexible multi-bodies. Keywords: Maneuvering flexible appendages; Equations of motion; Flexible structures; Control systems; Control laws; Line of sight; Spacecraft antennas/alignment; Vibration. (edc)


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    Control of large space structures

    JASPER, W. | AIAA | 1984


    Control of Large Flexible Space Structures

    Joshi, Suresh M. | TIBKAT | 1989


    Active control of large space structures

    Nebot, E.M. / Lee, G.K.F. / Brubaker, T.A. | Tema Archive | 1989


    Large space structures : dynamics and control

    Atluri, Satya N. ;Amos, A. K. | TIBKAT | 1988