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)
Control of Large Space Structures
1990
35 pages
Report
Keine Angabe
Englisch
Astronautics , Manned Spacecraft , Unmanned Spacecraft , Control systems , Spacecraft components , Alignment , Appendages , Control , Control theory , Equations of motion , Flexible structures , Grids(Coordinates) , Line of sight , Maneuverability , Spacecraft , Spacecraft antennas , Vibration , Large space structures , Flexible spacecraft , Articulate structures
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