Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
出版者
宇宙航空研究開発機構宇宙科学研究本部
出版者（英）
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)
雑誌名
アストロダイナミクスシンポジウム講演後刷り集
雑誌名(英)
Proceedings of 19th workshop on JAXA Astrodynamics and Flight Mechanics
Workshop on JAXA Astrodynamics and Flight Mechanics, 2009 (July 30-31, 2009. Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan
In ISAS/JAXA, a fully reusable vertical take-off and vertical landing (VTVL) sounding rocket is proposed as one step for the future full-fledged reusable transportation system. In landing phase, this vehicle makes a turnover maneuver from a nose-first entry attitude. This makes it possible to achieve the deceleration and soft landing by its main engine thrust. In this study, as for the inversion maneuver of the vertical landing vehicle, the aerodynamic turnover maneuver is considered. And the turnover maneuver for the nose first entry of the vehicle is numerically simulated and then the guidance strategy for the vehicle is considered.
内容記述
形態: カラー図版あり
内容記述（英）
Physical characteristics: Original contains color illustrations
Guidance Control of Attitude Turnover on Reentry Phase of Reusable Sounding Rocket
