Automatic landing flight experiment flight simulation analysis and flight testing

Toshikazu Motoda, Yoshikazu Miyazawa, Kazutoshi Ishikawa, Tatsushi Izumi

研究成果: Contribution to journalArticle査読

7 被引用数 (Scopus)

抄録

Preflight simulation analysis of flight experiment and flight test results are described. The automatic landing flight experiment was conducted in Woomera, Australia, in 1996, to develop the automatic landing technology required for the future Japanese uncrewed spacecraft. To ensure successful landings, computer simulation played an important role in the preflight analysis. Monte Carlo simulation was applied for the analysis. The root sum square method, which is commonly used in Japanese launcher rocket development projects, was also applied. Monte Carlo results were compared with the rss results and the flight test results. All 13 flight tests were successfully completed. Longitudinal guidance in the flare phase was found to be sensitive to some modeling errors. The cause is discussed.

本文言語英語
ページ(範囲)554-560
ページ数7
ジャーナルJournal of Spacecraft and Rockets
36
4
DOI
出版ステータス出版済み - 1 1 1999

All Science Journal Classification (ASJC) codes

  • 航空宇宙工学
  • 宇宙惑星科学

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