Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Ryoichi Takase"'
Publikováno v:
Machine Learning with Applications, Vol 10, Iss , Pp 100409- (2022)
In this study, two types of methods from different perspectives based on spectral normalization (SN) are described for ensuring the stability of a feedback system controlled by a neural network (NN). The first one is that the L2gain of the feedback s
Externí odkaz:
https://doaj.org/article/fbc6082c17f04918ad1454420b581b5d
Publikováno v:
SICE Journal of Control, Measurement, and System Integration, Vol 11, Iss 3, Pp 190-197 (2018)
This paper deals with a gust alleviation (GA) system using gain-scheduled (GS) discrete-time preview control. The key points to improve control performance of this system are in both modeling accuracy of the linear parameter-varying (LPV) system with
Externí odkaz:
https://doaj.org/article/54cbe1c2e27d482aaee2c7288af7fccc
Publikováno v:
Lecture Notes in Electrical Engineering ISBN: 9789811926341
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ccc7d95d0fd8851d1198f1c71bed4700
https://doi.org/10.1007/978-981-19-2635-8_64
https://doi.org/10.1007/978-981-19-2635-8_64
Publikováno v:
2022 61st Annual Conference of the Society of Instrument and Control Engineers (SICE).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9c6447d972e90bfa68b0d947f706acf8
https://doi.org/10.23919/sice56594.2022.9905772
https://doi.org/10.23919/sice56594.2022.9905772
Publikováno v:
IFAC-PapersOnLine. 53:14918-14923
This note presents the pilot assessment of a Fault-Tolerant Control (FTC) law for elevator efficiency reduction via Hardware-In-the-Loop Simulations (HILS) with a research airplane MuPAL-α. The FTC is supposed to be a PID controller from the viewpoi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a4e46dc65525b072865b8177790e441f
https://doi.org/10.1016/j.ifacol.2020.12.1959
https://doi.org/10.1016/j.ifacol.2020.12.1959
Publikováno v:
IFAC-PapersOnLine. 53:14833-14838
This article presents the design and evaluation of a robust C⁎ control law through Hardware-In-the-Loop Simulation (HILS) of JAXA’s research aircraft called Multi-Purpose Aviation Laboratory (MuPAL-α). The C⁎ control law, which is a widely use
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a08ef89a14bc6cdb3dbe3062f70ce2ec
https://doi.org/10.1016/j.ifacol.2020.12.1927
https://doi.org/10.1016/j.ifacol.2020.12.1927
Autor:
Shinji Suzuki, Yoshiro Hamada, Ryoichi Takase, Takashi Shimomura, Takeshi Tsuchiya, Kento Fujita
Publikováno v:
IFAC-PapersOnLine. 52:122-127
This paper presents robust control design for commercial aircraft, in which the control law is augmented with prior gust information. The main contribution of this paper is to integrate a gust alleviation system using Light Detection And Ranging (LID
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0492ef63597e94139ccd7ff4c61bb948
https://doi.org/10.1016/j.ifacol.2019.11.119
https://doi.org/10.1016/j.ifacol.2019.11.119
Publikováno v:
23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cd2f0ae44e86aa80a237cdb0dcd811e8
https://doi.org/10.2514/6.2020-2413
https://doi.org/10.2514/6.2020-2413
Publikováno v:
Aerospace Science and Technology. 106:106125
A piloted simulator evaluation is an important step for making a Fault-Tolerant Flight Control (FTFC) system more practical and reliable. Especially, in the case of an adaptive technique, conformance of the adaptive controller to the human pilot's in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6e8f2b9067ebdd5a4ce359fc37fe6023
https://doi.org/10.1016/j.ast.2020.106125
https://doi.org/10.1016/j.ast.2020.106125
Publikováno v:
ASCC
This paper deals with a fault-tolerant flight control system where the aircraft is manually controlled by pilots. Our previous research demonstrated that Simple Adaptive Control (SAC) with a PID compensator could automatically control an aircraft eve
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9b7e0968ae9f9e00f4efe31bc079bf53
https://doi.org/10.1109/ascc.2017.8287222
https://doi.org/10.1109/ascc.2017.8287222