Zobrazeno 1 - 10
of 22
pro vyhledávání: '"Toshikazu Motoda"'
Autor:
Toshikazu MOTODA1 motoda.toshikazu@jaxa.jp, Dongwon Jung
Publikováno v:
Transactions of the Japan Society of Aeronautical & Space Science. 2023, Vol. 66 Issue 6, p187-198. 12p.
Autor:
Toshikazu Motoda
Publikováno v:
Journal of Aerospace Information Systems.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::edb0063c372072b93a1beb61e4a70b8a
https://doi.org/10.2514/1.i010926.c1
https://doi.org/10.2514/1.i010926.c1
Autor:
Toshikazu Motoda
Publikováno v:
Journal of Aerospace Information Systems. 19(2)
Accepted: 2021-10-01
資料番号: PA2220002000
資料番号: PA2220002000
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6d6d401c36ed1b1a1751c89237981bd2
http://id.nii.ac.jp/1696/00049023/
http://id.nii.ac.jp/1696/00049023/
Autor:
Toshikazu Motoda
Publikováno v:
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 55:117-124
In aerospace projects preflight evaluation is crucial for mission success, because flight testing in a real environment is often difficult or impossible. Monte Carlo simulation is a powerful tool for the preflight evaluation because a nonlinear syste
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f9a8606330c3229ae2e2508897fee62a
https://doi.org/10.2322/jjsass.55.117
https://doi.org/10.2322/jjsass.55.117
Autor:
Toshikazu Motoda
Publikováno v:
Journal of Spacecraft and Rockets. 41:1071-1075
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e165f5cc28ac1d8d2b26dd3f2f21c02a
https://doi.org/10.2514/1.10265
https://doi.org/10.2514/1.10265
Autor:
Yoshikazu Miyazawa, Toshikazu Motoda
Publikováno v:
Journal of Spacecraft and Rockets. 39:615-623
Monte Carlo simulation is a powerful and a practical tool for evaluating nonlinear systems. Its advantage is that it allows the effects of combinations of uncertainties to be taken into account. When the result of a MonteCarlo simulation is unsatisfa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1e0b348fe43ee69a04d16762dd8e4562
https://doi.org/10.2514/2.3851
https://doi.org/10.2514/2.3851
Publikováno v:
Journal of Guidance, Control, and Dynamics. 25:267-274
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::695e9f13ba150430e7fa4a6407e52235
https://doi.org/10.2514/2.4878
https://doi.org/10.2514/2.4878
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference.
An airplane has been planned to be used for Mars exploration. The wing folding technology for such an airplane has been paid attention to because it offers a large wing area to get enough lift force and compactness for transfer to Mars. In addition,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1523f2c4a79d300b0a7cabea3ae54b7b
https://doi.org/10.2514/6.2014-0383
https://doi.org/10.2514/6.2014-0383
Autor:
Yoshikazu Miyazawa, Toshikazu Motoda
Publikováno v:
Journal of Guidance, Control, and Dynamics. 24:597-604
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::91372ea17d4e0b37c985ed43facbe2be
https://doi.org/10.2514/2.4751
https://doi.org/10.2514/2.4751
Publikováno v:
Journal of Guidance, Control, and Dynamics. 22:791-800
This paper discusses the longitudinal ight-pathcontrol lawdesigned and ight tested for theAutomaticLanding Flight Experiment (ALFLEX). ALFLEX, for which ight tests were conducted in 1996, demonstrated Japanese potential for developing automat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4f86e91d7ac95808684c9fa2f0b167d1
https://doi.org/10.2514/2.4480
https://doi.org/10.2514/2.4480