Spacecraft Attitude Control: A Consideration of Thrust Uncertainty
Author:
Affiliation:
1. Loyola University Chicago, Chicago, Illinois 60660
2. University of Illinois at Urbana–Champaign, Urbana, Illinois 61801
3. Georgia Institute of Technology, Atlanta, Georgia 30332
4. University of Waterloo, Waterloo, Ontario N2L 3G1, Canada
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.G005280
Reference23 articles.
1. Optimal stochastic control of linear systems with state- and control-dependent disturbances
2. Stochastic Hill's equations for the study of errant rocket burns in orbit
3. GustafsonE. D. “Stochastic Optimal Control of Spacecraft,” Ph.D. Dissertation, Aerospace Engineering Dept. Univ. of Michigan, Ann Arbor, MI, 2010.
4. Finite‐time attitude stabilisation for a class of stochastic spacecraft systems
5. On the optimal stabilization of nonlinear systems
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