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

Tomoya Sakamoto, Yuki Akiyama, Mai Bando, Shinji Hokamoto

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)

Abstract

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.

Original languageEnglish
Title of host publication2017 56th Annual Conference of the Society of Instrument and Control Engineers of Japan, SICE 2017
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages464-469
Number of pages6
Volume2017-November
ISBN (Electronic)9784907764579
DOIs
Publication statusPublished - Nov 10 2017
Event56th Annual Conference of the Society of Instrument and Control Engineers of Japan, SICE 2017 - Kanazawa, Japan
Duration: Sep 19 2017Sep 22 2017

Other

Other56th Annual Conference of the Society of Instrument and Control Engineers of Japan, SICE 2017
CountryJapan
CityKanazawa
Period9/19/179/22/17

All Science Journal Classification (ASJC) codes

  • Computer Science Applications
  • Control and Optimization
  • Control and Systems Engineering
  • Instrumentation

Fingerprint Dive into the research topics of 'Considerations on design parameters for attitude control of spacecraft using port-controlled Hamiltonian systems'. Together they form a unique fingerprint.

  • Cite this

    Sakamoto, T., Akiyama, Y., Bando, M., & Hokamoto, S. (2017). Considerations on design parameters for attitude control of spacecraft using port-controlled Hamiltonian systems. In 2017 56th Annual Conference of the Society of Instrument and Control Engineers of Japan, SICE 2017 (Vol. 2017-November, pp. 464-469). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.23919/SICE.2017.8105722