Investigated are the dynamics and control of high-order dynamical systems as used in flexible spacecraft. The procedure adopted is referred to as modal-space control and consists of a scheme for independent control of spacecraft modes. The basic idea behind this method is that the control laws are first designed in the modal-space for each independent set in a way that the response of one pair of modes does not effect those of any other pair. The approach makes a design of nonlinear on-off control laws as well as proportional control of high-order system possible. (de Posamentier)
Dynamics and control in modal-space of flexible spacecraft
Dynamik und Steuerung komplexer Systeme in flexiblen Raumfahrzeugen
1979
191 Seiten
Hochschulschrift
Englisch
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