Toward Uncertainty Quantification in Satellite Thermal Design
Author:
Affiliation:
1. Research and Development Directorate, JAXA
2. Space Technology Directorate I, JAXA
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/tastj/17/2/17_17.134/_pdf
Reference14 articles.
1. 1) JERG-2-310 Spacecraft Thermal Control System, Japan Aerospace Exploration Agency, Tokyo, http://sma.jaxa.jp/en/ TechDoc/Docs/E_JAXA-JERG-2-310_08_RE.pdf (accessed April 12, 2017).
2. 2) Díaz J. and Hernández, H.: Uncertainty quantification and robust design of aircraft components under thermal loads, Aerospace Science and Technology, 14 (2010), No. 8, pp. 527-534.
3. 3) Aleksandr, C., Simon, R. P., and Richard L.: Uncertainty Quantification in Multiscale Simulation of Materials: A Prospective, Annual Review of Materials Research, 43 (2013), pp. 157-182.
4. 4) Pecnik, R., Witteveen, J., and Iaccarino, G.: Uncertainty quantification for laminar-turbulent transition prediction in RANS turbomachinery applications, Proceedings of 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, 2011, AIAA 2011-660.
5. 5) Akita, T., Takaki, R., and Shima, E.: An Estimation Method of Thermal Contact Resistances in Satellite Thermal Model by Using the Ensemble Kalman Filter, AEROSPACE TECHNOLOGY JAPAN, 9 (2010), pp. 1-8 (in Japanese).
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