Attitude Control of Space Launch Vehicles by Using Model Predictive Control
Author:
Affiliation:
1. School of Physical Sciences, The Graduate University for Advanced Studies
Publisher
The Society of Instrument and Control Engineers
Link
https://www.jstage.jst.go.jp/article/sicetr/58/3/58_168/_pdf
Reference14 articles.
1. 1) 森田，川口，後藤：M-Vダイナミクスと姿勢制御論理の設計，宇宙科学研究所報告特集，47, 141/154 (2003)
2. 2) S. Dey, D.K. Giri, V. Laxmi and A.K. Ghosh: Time-Varying Non-Singular Terminal Sliding Mode Attitude Control of Reusable Launch Vehicle, 15th International Conference on Control, Automation, Robotics and Vision, 984/989 (2018)
3. 3) D. Trotta, A. Zavoli and G.D. Matteis: Optimal Tuning of Adaptive Augmenting Controller for Launch Vehicles in Atmospheric Flight, Journal of Guidance, Control, and Dynamics, 43-11, 2133/2140 (2020)
4. 4) J.P.B. Araque, A. Zavoli, D. Trotta and G.D. Matteis: Genetic Algorithm Based Parameter Tuning for Robust Control of Launch Vehicle in Atmospheric Flight, IEEE Access, 9, 108175/108189 (2021)
5. 5) L. Zhang, C. Wei, R. Wu and N. Cui: Adaptive Fault-Tolerant Control for a VTVL Reusable Launch Vehicle, Acta Astronautica, 159, 362/370 (2019)
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