Nonlinear model predictive control applied to spacecraft attitude control (Closed-loop stability and optimality with thrusters and wheels)

Atsushi SAKAMOTO, Yuichi IKEDA, Isao YAMAGUCHI, Takashi KIDA

Open source

DOI: 10.1299/transjsme.16-00198
Published: 10
Container: Nihon Kikai Gakkai ronbunshu
Publisher: Not recorded
Open access: yes

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Cite this work

BibTeX

@article{allodium:10.1299/transjsme.16-00198,
  title = {Nonlinear model predictive control applied to spacecraft attitude control (Closed-loop stability and optimality with thrusters and wheels)},
  author = {Atsushi SAKAMOTO and Yuichi IKEDA and Isao YAMAGUCHI and Takashi KIDA},
  year = {2016},
  journal = {Nihon Kikai Gakkai ronbunshu},
  doi = {10.1299/transjsme.16-00198},
  url = {https://doi.org/10.1299/transjsme.16-00198}
}

RIS

TY  - JOUR
TI  - Nonlinear model predictive control applied to spacecraft attitude control (Closed-loop stability and optimality with thrusters and wheels)
AU  - Atsushi SAKAMOTO
AU  - Yuichi IKEDA
AU  - Isao YAMAGUCHI
AU  - Takashi KIDA
PY  - 2016
JO  - Nihon Kikai Gakkai ronbunshu
DO  - 10.1299/transjsme.16-00198
UR  - https://doi.org/10.1299/transjsme.16-00198
ER  -

APA

SAKAMOTO, A., IKEDA, Y., YAMAGUCHI, I., & KIDA, T. (2016). Nonlinear model predictive control applied to spacecraft attitude control (Closed-loop stability and optimality with thrusters and wheels). Nihon Kikai Gakkai ronbunshu. https://doi.org/10.1299/transjsme.16-00198

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doaj · retrieved 2026-09-26T09:42:55.945Z