Nonlinear and linear equations of motions were derived. The preliminary investigation consisted of model beam as truss structure, effects of truss structure on control design, and effects of reflector offset on control design. It was concluded that the offset of the reflector c.g. from the beam reflector attach point is dynamically significant. Also, truss effects may also significantly effect the performance of the controller if ignored. If the truss is included in the modeling of the NASA/SCOLE configuration, a practically implementable scheme is available to reduce the model order.
Modelling issues of the SCOLE control problem
01.01.1984
Aufsatz (Konferenz)
Keine Angabe
Englisch
NTRS | 1987
|NTRS | 1987
|Maneuver and vibration control of SCOLE
NTRS | 1988
|Maneuver and vibration control of SCOLE
AIAA | 1986
|Maneuver and vibration control of SCOLE
NTRS | 1986
|