@inproceedings{oai:jaxa.repo.nii.ac.jp:00038614,
 author = {服部, 和恵 and 林, 健太郎 and 横田, 清美 and Hattori, Kazue and Hyashi, Kentaroh and Yokota, Kiyomi},
 book = {第57回宇宙科学技術連合講演会講演集, Proceedings of 57th Space Sciences and Technology Conference},
 month = {Oct},
 note = {第57回宇宙科学技術連合講演会（2013年10月9日-11日. 米子コンベンションセンター（BiG SHiP）), 米子市, 鳥取県, The ascent guidance of a launch vehicle is generally applied in exo-atmospheric phase. Japanese next generation launchvehicle, H-3 is considered to fly in atmospheric phase relatively long time compared to current workhorse H-IIA rocket.This means that the first stage guidance duration of H-3 could be shorter than H-IIA, trajectory dispersion be bigger, morepropellant be used. To solve this problem, simplified endo-atmospheric guidance is proposed. This guidance can beapplied in atmospheric phase, and also execution time with on-board computer may well be reasonable. This paperdescribes the proposed guidance and simulation results., 資料番号: AC1400030000, レポート番号: JSASS-2013-4109},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences(JSASS)},
 title = {次期基幹ロケットを想定した大気中誘導の検討},
 year = {2013}
}