@inproceedings{oai:jaxa.repo.nii.ac.jp:00007334,
 author = {山本, 高行 and 野中, 聡 and Yamamoto, Takayuki and Nonaka, Satoshi},
 book = {アストロダイナミクスシンポジウム講演後刷り集, Proceedings of 19th workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {アストロダイナミクスシンポジウム (2009年7月30-31日. 宇宙航空研究開発機構宇宙科学研究本部)), 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, 垂直離着陸を行う再使用観測ロケットでは，帰還時に頭部から降下し，着陸前に姿勢転回を行うことを検討している．本研究では，空力特性を利用して姿勢転回を行う際の誘導制御を検討するため，帰還時の数値シミュレーションを行う．, 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., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064734029},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)},
 title = {Guidance Control of Attitude Turnover on Reentry Phase of Reusable Sounding Rocket},
 volume = {2009},
 year = {2010}
}