Flight Control Parameter Design for Mars Airplane Balloon Experiment-1 (MABE-1) Using Evolutionary Computation

Author:

FUJITA Koji1,TOKUTAKE Hiroshi2,NAGAI Hiroki3,OYAMA Akira1

Affiliation:

1. Institute of Space and Astronautical Science, JAXA

2. Kanazawa University

3. Institute of Fluid Science, Tohoku University

Publisher

Japan Society for Aeronautical and Space Sciences

Reference10 articles.

1. 1) Nagai, H. and Oyama, A.: Development of Japanese Mars Airplane, Proceedings of the 67th International Astronautical Congress, IAC-16-A3.3A.5x35104, Guadalajara, Mexico, Sep. 2016.

2. 2) Oyama, A., Nagai, H., Tokutake, H., Fujita, K., Anyoji, M., Toyota, H., Miyazawa, Y., Yonemoto, K., Okamoto, M., Nonomura, T., Motoda, T., Takeuchi, S., Kamata, Y., Otsuki, M., Asai, K. and Fujii, K.: Flight System of Mars Airplane Balloon Experiment-1 (MABE-1), Proceedings of the 31st International Symposium on Space Technology and Science, 2017-k-42, June. 3-9, 2017.

3. 3) Oyama, A., Nagai, H., Tokutake, H., Fujita, K., Anyoji, M., Toyota, H., Miyazawa, Y., Yonemoto, K., Okamoto, M., Nonomura, T., Motoda, T., Takeuchi, S., Kamata, Y., Otsuki, M., Asai, K. and Fujii, K.: Aerodynamic Data Acquisition of Mars Airplane by High Altitude Flight Test, JAXA Research and Development Report Research, Reports on High Altitude Balloons, JAXA-RR-16-008, 2017 (in Japanese).

4. 4) Porter, B. and Jones, A. H.: Genetic Tuning of Digital PID Controllers, Electronics Letter, 28 (1992), 843/844 10.

5. 5) Krishnakumar, K. and Goldberg, D. E.: Control System Optimization Using Genetic Algorithm, J. Guidance, Control, and Dynamics, 15 (1992), pp.735-740.

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