Fuel Slosh Dynamics in Spinning Spacecraft
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Publisher
American Institute of Aeronautics and Astronautics
Reference12 articles.
1. Slater, L. I., and Smay, J. W. "Comstar Spacecraft Product-of-Inertia Coupled Electronic Nutation Damper." Guidance and Control Conference, Hollywood, FL, August8-10,1977,1977, p.137-145.(AIAA-1977-1056)
2. Smay, J. W. and Slater, L. I. "Dual-spin spacecraft stabilization using nutation feedback and inertia coupling" JOURNALOF SPACECRAFT AND ROCKETS 1976, vol.13no.11(650-659)
3. Odhekar,D.D.,Gandhiy,P. S.andJoshiz,K.B.,NovelMethodsforSloshParameterEstimationUsingPendulum Analogy. AIAA Atmospheric Flight Mechanics Conference and Exhibit, 15 - 18 August 2005, San Francisco, California, AIAA2005-5923.
4. Schlee, K., Gangadharan, S. and Ristow, J. Sudermann, J. and Walker, C. and Hubert, C. "Advanced Method to Estimate Fuel Slosh Simulation Parameters" 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Tucson, Arizona, July10-13,2005(AIAA-2005-3596)
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