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A class of stable, robust feedback controllers for large space structuresA two-level control system design is considered for large space structures, which consists of a primary and a secondary controller. The secondary or damping enhancement controller is shown to be stable and robust, even when time-invariant nonlinearities are present in the actuators and/or sensors. The use of Annular Momentum Control Devices (AMCD's) is also considered for secondary control. The primary attitude controller using collocated torque actuators and attitude and rate sensors is stable and robust. The effect of actuator/sensor dynamics on the stability of the primary and secondary controllers is considered. The AMCD's used for secondary control actuation can also be used for the primary controller.
Document ID
19810063063
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Joshi, S. M.
(Old Dominion University Research Foundation, Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
September 1, 1981
Subject Category
Spacecraft Instrumentation
Report/Patent Number
IAF PAPER 81-351
Report Number: IAF PAPER 81-351
Accession Number
81A47467
Funding Number(s)
CONTRACT_GRANT: NAG1-102
Distribution Limits
Public
Copyright
Other

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