Stability Margin Evaluation of DI Control System for Suborbital Spaceplane During Re-entry Phase

Author:

Watanabe Tomotaka,Yonemoto Koichi,Fujikawa Takahiro,Matsukami Takahiro

Publisher

Springer Nature Singapore

Reference6 articles.

1. Fujikawa, T., Yonemoto, K.: Application of multidisciplinary design optimization to the development of an unmanned suborbital spaceplane by industry-government-academia collaboration. In: 73rd International Astronautical Congress (2022)

2. Lane, S.H., Stengel, R.F.: Flight control design using non-linear inverse dynamics. Automatica 24, 471–483 (1988)

3. Kawaguchi, J., Suzuki, H., et al.: Post-flight evaluation of the guidance and control for D-SEND#2 2nd drop test. In: AIAA Atmospheric Flight Mechanics Conference (2017)

4. Shirakata, K., Yonemoto, K., Fujikawa, T.: Flight attitude controller using dynamic inversion theory with stability margin guarantee. Int. J. Eng. Res. Appl. 8, 16–27 (2018)

5. Fujikawa, T., Yonemoto, K.: Application of multidisciplinary design optimization to preliminary design of suborbital spaceplane. In: 33rd International Symposium on Space Technology and Science (2022)

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