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Flexible stator control on the Galileo spacecraftGalileo is a dual-spin spacecraft designed to deliver a probe to Jupiter and then orbit the planet. The stator, or despun section, contains four flexible modes below 10 Hz and the despun actuator is separated from the inertial sensors by this flexibility. Control loop separation by bandwidth proved unacceptable due to performance requirements. To obtain the desired performance, a control scheme was devised which consists of three parts. First, flexibility damping and control notch filtering are accomplished by phase locked loop techniques. Second, slewing maneuvers are produced by torque profiles which are nonexcitatory to the structure. Finally, a low bandwidth perturbation controller is supplied to remove spacecraft disturbances.
Document ID
19790063225
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kopf, E. H.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Brown, T. K.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Marsh, E. L.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 9, 2013
Publication Date
June 1, 1979
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AAS PAPER 79-161
Meeting Information
Meeting: American Astronautical Society and American Institute of Aeronautics and Astronautics, Astrodynamics Specialist Conference
Location: Provincetown, MA
Start Date: June 25, 1979
End Date: June 27, 1979
Sponsors: American Astronautical Society, American Institute of Aeronautics and Astronautics
Accession Number
79A47238
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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