Application of MPC to Spacecraft Attitude Maneuver using RCS and/or RW

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概要

• 論文の詳細を見る

• 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 stability framework and derive a stability condition described by a linear matrix inequality (LMI). Some numerical studies are performed and the effectiveness of the proposed model predictive control is shown.

• 一般社団法人 日本機械学会の論文

著者

• Kida Takashi

  University Of Electro-communications

• ASAKAWA Takeya

  University of Electro-Communications

関連論文

• Optimal Static Output Feedback Control for Large Space Structures and Its Application to Local Control
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• In-orbit Control Experiment on ETS-VIII Spacecraft
• Application of MPC to Spacecraft Attitude Maneuver using RCS and/or RW
• Robust Attitude Control Using Mu-Synthesis for the Large Flexible Satellite ETS-VIII

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