@techreport{oai:jaxa.repo.nii.ac.jp:00041465,
 author = {鈴木, 広一 and 吉田, 憲司 and 真保, 雄一 and 大貫, 武 and Suzuki, Hirokazu and Yoshida, Kenji and Shinbo, Yuichi and Onuki, Takeshi},
 month = {Jan},
 note = {本稿では、第1報(NAL TR-1377(航空宇宙技術研究所技術レポート-1377))による検討結果を受けて、ロケット打ち上げによる小型超音速実験機の航法・誘導則と飛行実験計画を発展、改良した結果について述べる。具体的には、第1報で策定した第2次飛行実験計画を成立させるため、航法計算周期を改善し、新たに目標動圧追従型の誘導則を設計して航法・誘導・制御システムの機能強化を図った。このシステムを用いて第2次飛行実験計画案について検討した結果、実験計画成立の見通しが得られた。よって、第2次飛行実験計画案を、ロケット実験機基本設計に於けるNALの最終的な飛行実験計画案として設定した。, Two types of scaled supersonic experimental airplanes, an unpowered and a jet propelled vehicle, are now being developed in order to establish advanced technologies for the development of a second generation supersonic transport. The first author reports the basic system of guidance, navigation and control and the first flight experiment plan for the unpowered experimental airplane in NAL TR-1377. The guidance and navigation system were improved to enable the system to action the second flight experiment plan which was newly defined as a result of investigations conducted for the first flight experiment plan. The calculation frequency of the major cycle of the navigation law rose higher to improve the performance of the attitude control. The function of tracking the target dynamic pressure was newly added to the guidance law. The new guidance, navigation and control system had sufficient ability to ensure the second flight experiment was carried out successfully. The second experiment flight plan was therefore proposed as NAL's final flight plan in the definition study phase., 資料番号: AA0028640000, レポート番号: NAL TM-746},
 title = {小型超音速実験機の航法・誘導則と飛行実験計画に関する検討　第2報},
 year = {2000}
}