Extra-insensitive input shapers for controlling flexible spacecraft

A procedure for designing command profiles for flexible spacecraft is presented. The command profiles are required to move a spacecraft from rest to rest or to accelerate a spacecraft to a constant velocity with very little residual vibration. To model the case where the spacecraft is equipped with...

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Veröffentlicht in:Journal of guidance, control, and dynamics control, and dynamics, 1996-03, Vol.19 (2), p.385-391
Hauptverfasser: Singhose, William, Derezinski, Steve, Singer, Neil
Format: Artikel
Sprache:eng
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