入力拘束を考慮したモデル予測制御の柔軟衛星への適用

山下 哲生; 濱田 吉郎; 山口 功; 木田 隆; 長塩 知之

doi:10.11511/jacc.53.0.255.0

THE 53RD JAPAN JOINT AUTOMATIC CONTROL CONFERENCE

Session ID : 532

DOI https://doi.org/10.11511/jacc.53.0.255.0

Conference information

Host: The Japan Society of Mechanical Engineers, The Society of Instrument and Control Engineers, The Institute of Systems, Control and Information Engineers, The Society of Chemical Engineers, Japan, The Japan Society for Precision Engineering, The Japan Society for Aeronautical and Space Sciences

Co-host: Technically Cosponsored by 50 Societies and Institutes

Guidance and Control in Aerospace Engineering 1

Application of Input Constrained Model Predictive Control to Flexible Spacecraft

*Tetsuo Yamashita, Yoshiro Hamada, Isao Yamaguchi, Takashi Kida, Tomoyuki Nagashio

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Keywords: Model Predictive Control, Input-constraint, Flexible spacecraft, Attitude control

CONFERENCE PROCEEDINGS FREE ACCESS

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Abstract

This paper studies to apply the model predictive control to flexible spacecraft attitude maneuver. We aim to obtain the optimal attitude controller suppressing the flexible appendage vibration under the actuator saturation. Through numerical simulations, its ability is shown.

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