Výsledky vyhledávání - "Miyazawa, Yoshikazu"

Publikováno v: 宇宙航空研究開発機構特別資料: 平成23年度JAXA航空プログラムグループ公募型研究報告会資料集（22年度採用分） = JAXA Special Publication: Proceedings of FY2011 debriefing session on research and development promotion program of JAVA Aviation Program Group. :81-90

形態: カラー図版あり
Physical characteristics: Original contains color illustrations
Translation title: Study on the flight path of free-fall supersonic flying object dropped down from balloon: Optimization of flight path by dynami

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::64bb760ea8df13aa6f820f5f1359dec8
http://id.nii.ac.jp/1696/00004283/

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Study on the flight path of free-fall supersonic flying object dropped down from balloon: Optimization of flight path by dynamic programming

Autor: Miyazawa, Yoshikazu

Publikováno v: 宇宙航空研究開発機構特別資料: 平成22年度JAXA航空プログラムグループ公募型研究報告会資料集 = JAXA Special Publication. :125-131

平成22年度JAXA航空プログラムグループ公募型研究報告会 (2010年11月26日. 宇宙航空研究開発機構)
Debriefing session on research and development promotion program of JAVA Aviation Program Group (November 26, 2010. J

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::69e7b5226e6a9b2ee79ab4699bb7e643
http://id.nii.ac.jp/1696/00004634/

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Design and Evaluation of a Flight Control Law Using the Hierarchy-structured Dynamic Inversion Approach

Autor: Kawaguchi, Junichiro, Miyazawa, Yoshikazu, Ninomiya, Tetsujiro

Publikováno v: 計測自動制御学会論文集 = Transactions of the Society of Instrument and Control Engineers. 45(12):703-710

資料番号: PA0910102000

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::aa17af8ae5fa057ab6f16dbb342d4fd5
http://id.nii.ac.jp/1696/00022056/

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Results of actual flight and evaluation for guidance and control system of high speed flight demonstration phase 2

Autor: Suzuki, Hirokazu, Tsukamoto, Taro, Ninomiya, Tetsujiro, Miyazawa, Yoshikazu

Publikováno v: 宇宙輸送シンポジウム平成15年度 = Proceedings of Space Transportation Symposium FY2003. :186-189

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 eva

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::fd04a63775867795e6f74d890f9987dd
http://id.nii.ac.jp/1696/00017271/

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Phase 1 flight experiment of high speed flight demonstration

Autor: Sarae, Wataru, Nishizawa, Takeshi, Sagisaka, Masakazu, Akimoto, Toshio, Miyazawa, Yoshikazu, Yanagihara, Masaaki

Publikováno v: 宇宙輸送シンポジウム平成14年度 = Proceedings of Space Transportation Symposium FY2002. :177-180

宇宙開発事業団と航空宇宙技術研究所では将来の再使用型宇宙輸送システム開発に必要な技術蓄積を図るための共同研究を実施しており、その一環として高速飛行実証計画を進めている�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::3a6c0e925fdf46e11af576667deb3d2e
http://id.nii.ac.jp/1696/00017374/

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Present status and problems of transonic CFD validation for High Speed Flight Demonstrator Phase 2 flight experiment

Autor: Yamamoto, Yukimitsu, Ueno, Makoto, Yanagihara, Masaaki, Miyazawa, Yoshikazu, Ito, Ryozo

Publikováno v: 航空宇宙技術研究所特別資料: 航空宇宙数値シミュレーション技術シンポジウム2002論文集 = Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2002. 57:144-147

Computational analysis of High Speed Flight Demonstrator (HSFD) Phase 2 Vehicle are presented. HSFD Phase 2 is the flight experiment to reduce uncertainties in the HOPE-X transonic aerodynamics. HSFD vehicle is 25 percent scale model of HOPE-X. The p

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::9dd0835abd28f7fc74857a08421fe074
http://id.nii.ac.jp/1696/00038241/

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