Zobrazeno 1 - 10
of 24
pro vyhledávání: '"Tetsujiro Ninomiya"'
Autor:
Tetsujiro Ninomiya, Masaru Naruoka, Takahiro Uchiyama, Kento Yamada, Makoto Ueno, Hideyuki Sawada
Publikováno v:
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 71:1-11
Publikováno v:
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 70:58-66
Publikováno v:
Transactions of the Japan Society for Aeronautical and Space Sciences. 63(6):257-264
形態: カラー図版あり
Physical characteristics: Original contains color illustrations
Accepted: 2020-06-15
資料番号: PA2120008000
Physical characteristics: Original contains color illustrations
Accepted: 2020-06-15
資料番号: PA2120008000
Publikováno v:
Transactions of the Japan Society for Aeronautical and Space Sciences. 61(6):248-257
Physical characteristics: Original contains illustrations
Accepted: 2018-05-15
資料番号: PA1920002000
Accepted: 2018-05-15
資料番号: PA1920002000
Publikováno v:
IFAC-PapersOnLine. 49:106-111
Release from a high-altitude balloon is a cost-effective means of achieving supersonic flight, but there have been only two prior applications of this method to aircraft flight testing. The Japanese Aerospace Exploration Agency’s D–SEND#2 flight
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference.
Publikováno v:
Journal of Guidance, Control, and Dynamics. 34:1573-1576
Autor:
Tetsujiro Ninomiya, Yoshikazu Miyazawa
Publikováno v:
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 58:219-225
More and more UAVs are developed for various purposes and their flight controllers are required to have sufficient robustness and performance to realize their versatile missions. To design these sophisticated controller is pretty much time-consuming
Publikováno v:
Journal of Spacecraft and Rockets. 43:1423-1426
T HE Japan Aerospace Exploration Agency (JAXA) has been researching key technologies for future space transportation. A series of flight experiments have been carried out to develop technologies for the planned H-II orbiting plane experimental (HOPE-
Publikováno v:
Journal of Guidance, Control, and Dynamics. 29:20-24
A new systematic method to design a control law for a linear system with a nonlinear input is proposed. Conventionally, the inverse of the nonlinear function is often used to such problems, but it requires too much calculation to solve the nonlinear