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Application of MPC to Spacecraft Attitude Maneuver using RCS and/or RW
2013
Journal of Space Engineering
This paper applies model predictive control (MPC) to multi-input spacecraft attitude maneuver problems using reaction control systems (RCS) and reaction wheels (RW). For this purpose, we consider linear quadratic cost functions under the input constraints of nonlinear on-off control inputs for RCS and linear continuous inputs with saturation for RW. These are optimized as mixed integer quadratic programming (MIQP) problems. We further analyze the closed-loop stability in the input-to-state
doi:10.1299/spacee.6.1
fatcat:sycqiawqpvbydov4kmzg22e6qa