Fully-Coupled Dynamical Jitter Modeling of a Rigid Spacecraft with Imbalanced Reaction Wheels
Author:
Affiliation:
1. University of Colorado, Boulder
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-5686
Reference13 articles.
1. 1Dewell, L., Pedreiro, N., Blaurock, C., Liu, K.C., Alexander, J., and Levine, M. “Precision Telescope Pointing and Spacecraft Vibration IsolationfortheTerrestrialPlanetFinderCoronagraph,”SPIESpaceTelescopeOptomechanicsandDynamics,2005.
2. 2Rizzo,M.J.,Rinehart,S.,Alcorn,J.,Barry,R.,Benford,D.,Fixsen,D.,etal.“BuildingAnInterferometerAtTheEdgeOfSpace: Pointing AndPhaseControlSystemForBETTII,”SPIESpaceTelescopesandInstrumentation,2014.
3. 3Masterson,R.andMiller,D.“DevelopmentofEmpiricalandAnalyticalReactionWheelDisturbanceModels,”AIAAStructures,Structural Dynamics,andMaterials,1999.
4. 5Liu,L.“JitterAndBasicRequirementsOfTheReactionWheelAssemblyInTheAttitudeControlSystem,”2007.
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