Random Generation of Aerodynamic Derivatives for Monte Carlo Evaluation-Reference-Cited by-同舟云学术

Random Generation of Aerodynamic Derivatives for Monte Carlo Evaluation

Published:2023 Issue:6 Volume:66 Page:187-198
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

MOTODA Toshikazu¹

Affiliation:

1. Aviation Technology Directorate, Japan Aerospace Exploration Agency

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/66/6/66_T-23-08/_pdf

Reference26 articles.

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3. 3) Ninomiya, T., Suzuki, H., and Tsukamoto, T.: Evaluation of Guidance and Control Systems of a Balloon-Launched Drop Test Vehicle, J. Spacecr. Rockets, 43, 6 (2006), pp. 1423–1425. https://doi.org/10.2514/1.23265

4. 4) Ninomiya, T., Suzuki, H., and Kawaguchi, J.: Dynamic Inversion Controller Design for Balloon-Launched Supersonic Aircraft, Trans. Jpn. Soc. Aeronaut. Space Sci., 61, 6 (2018), pp. 248–257. https://doi.org/10.2322/tjsass.61.248

5. 5) Schubert, W. M. and Stengel, R. F.: Parallel Synthesis of Robust Control Systems, IEEE Trans. Control Syst. Technol., 6, 6 (1998), pp. 701–706. https://doi.org/10.1109/87.726531