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Proceedings Paper

Precision control moment gyroscope spacecraft control with disturbance
Author(s): Christopher J. Heiberg; David Bailey; Bong Wie
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Paper Abstract

Standard feedback control systems subjected to periodic disturbances often cannot avoid sustained oscillatory responses at the disturbance frequency. Periodic disturbance rejection in a feedback control system via the insertion of an oscillator in the controller (internal model principle) is an effective method and well understood. By proper pole-zero placement, stable, steady-state performance which asymptotically approaches zero is achieved through the application of this type of filter. When the periodic disturbance is variable in frequency, the application of this type of filter is achieved by allowing the oscillator frequency to follow the disturbance. This, however, presents several problems in the actual application. This paper describes two applications of a variable periodic disturbance rejection filter in a spacecraft attitude control system and discusses the problems encountered and areas of further research.

Paper Details

Date Published: 6 June 1997
PDF: 12 pages
Proc. SPIE 3041, Smart Structures and Materials 1997: Smart Structures and Integrated Systems, (6 June 1997); doi: 10.1117/12.275722
Show Author Affiliations
Christopher J. Heiberg, Honeywell Satellite Systems (United States)
David Bailey, Honeywell Satellite Systems (United States)
Bong Wie, Arizona State Univ. (United States)


Published in SPIE Proceedings Vol. 3041:
Smart Structures and Materials 1997: Smart Structures and Integrated Systems
Mark E. Regelbrugge, Editor(s)

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