@inproceedings{oai:jaxa.repo.nii.ac.jp:00017277,
 author = {鈴木, 広一 and 塚本, 太郎 and 二宮, 哲次郎 and 宮沢, 与和 and Suzuki, Hirokazu and Tsukamoto, Taro and Ninomiya, Tetsujiro and Miyazawa, Yoshikazu},
 book = {宇宙輸送シンポジウム　平成15年度, Proceedings of Space Transportation Symposium FY2003},
 month = {Apr},
 note = {The high speed flight demonstration phase 2 was performed under cooperation of NAL, NASDA and CNES at Esrange in Sweden on July 1st, 2003. The purpose of this paper is to describe evaluation for the guidance and control system of the vehicle. The evaluation was executed by two approaches, a normal analysis and a special analysis. Although some cases of the Monte-Carlo simulation that is a part of the normal analysis could not satisfy mission requirements, detailed analysis of them says the system would lead the vehicle to successful flight experiment. The guidance and control system is graded by actual flight data, and it is cleared that the system satisfied all of the mission requirements. Based on the results of the preflight and the post-flight evaluation, this paper concludes that the design and evaluation for the guidance and control system of the vehicle were properly carried out., 資料番号: AA0047118047},
 pages = {186--189},
 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/ISAS)},
 title = {高速飛行実証フェーズ2の誘導制御系と実飛行結果},
 year = {2004}
}