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Single Axis Attitude Control and DC Bus Regulation with Two FlywheelsA computer simulation of a flywheel energy storage single axis attitude control system is described. The simulation models hardware which will be experimentally tested in the future. This hardware consists of two counter rotating flywheels mounted to an air table. The air table allows one axis of rotational motion. An inertia DC bus coordinator is set forth that allows the two control problems, bus regulation and attitude control, to be separated. Simulation results are presented with a previously derived flywheel bus regulator and a simple PID attitude controller.
Document ID
20020082945
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Kascak, Peter E. (Toledo Univ. OH United States)
Jansen, Ralph H. (Toledo Univ. OH United States)
Kenny, Barbara (NASA Glenn Research Center Cleveland, OH United States)
Dever, Timothy P. (QSS Group, Inc. Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 2002
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-13507
NAS 1.15:211812
IECEC-2002-20078
NASA/TM-2002-211812
Report Number: E-13507
Report Number: NAS 1.15:211812
Report Number: IECEC-2002-20078
Report Number: NASA/TM-2002-211812
Meeting Information
Meeting: 37th Intersociety Energy Conversion Engineering Conference
Location: Washington, DC
Country: United States
Start Date: June 28, 2002
End Date: August 2, 2002
Sponsors: Institute of Electrical and Electronics Engineers, Electron Devices Society
Funding Number(s)
PROJECT: RTOP 755-1A-09
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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