Control system synthesis for a launch vehicle with severe mode interaction

The phenomenon of mode interaction between rigid-body and elastic motion of a large launch vehicle is described and illustrated. For severe interaction, control system synthesis by the usual approach of assuming pitch attitude and rate feedback and use of conventional servo analysis techniques is no...

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Veröffentlicht in:	IEEE transactions on automatic control 1969-10, Vol.14 (5), p.517-523
1. Verfasser:	Swaim, R.
Format:	Artikel
Sprache:	eng
Schlagworte:	Attitude control Control system synthesis Control theory Damping Error correction Feedback Frequency Servomechanisms Signal synthesis Vehicle dynamics
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