Considerations on design parameters for attitude control of spacecraft using port-controlled Hamiltonian systems

Tomoya Sakamoto, Yuki Akiyama, Mai Bando, Shinji Hokamoto

研究成果: Chapter in Book/Report/Conference proceedingConference contribution

1 被引用数 (Scopus)

抄録

In previous research, a controller design procedure via generalized canonical transformations has been proposed to keep the passivity feature of Port-controlled Hamiltonian systems. The procedure has a general form and is applicable to spacecraft's attitude motion described with quaternion parameters. This paper investigates the roles of several design parameters in the generalized canonical transformations. Special attention is placed on the relation between the shape of Lyapunov functions and the convergence speed of the state variables. Furthermore, from the analysis utilizing the linearized form of the Port-controlled Hamiltonian system, the guideline to decide the preferable ratio between two parameters in the design procedure is proposed.

本文言語英語
ホスト出版物のタイトル2017 56th Annual Conference of the Society of Instrument and Control Engineers of Japan, SICE 2017
出版社Institute of Electrical and Electronics Engineers Inc.
ページ464-469
ページ数6
2017-November
ISBN(電子版)9784907764579
DOI
出版ステータス出版済み - 11 10 2017
イベント56th Annual Conference of the Society of Instrument and Control Engineers of Japan, SICE 2017 - Kanazawa, 日本
継続期間: 9 19 20179 22 2017

その他

その他56th Annual Conference of the Society of Instrument and Control Engineers of Japan, SICE 2017
国/地域日本
CityKanazawa
Period9/19/179/22/17

All Science Journal Classification (ASJC) codes

  • コンピュータ サイエンスの応用
  • 制御と最適化
  • 制御およびシステム工学
  • 器械工学

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