Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Moon Gyeang Cho"'
Publikováno v:
International Journal of Aerospace Engineering, Vol 2021 (2021)
This paper investigates the adaptive incremental backstepping sliding mode control for the rotorcraft trajectory-tracking control problem to enhance the robustness to the matched uncertainty in the model. First, the incremental dynamics is used for t
Externí odkaz:
https://doaj.org/article/40f0d6cd41f6432490205d0cb203f9c6
Publikováno v:
International Journal of Aerospace Engineering, Vol 2022 (2022)
This paper investigates an adaptive backstepping control based on the immersion-and-invariance (I&I) method for a rotorcraft’s trajectory-tracking control problem. To effectively cope with both parametric uncertainties and external disturbances aff
Externí odkaz:
https://doaj.org/article/74fbb29564604bf7bfc95db4567f5f77
Publikováno v:
Aerospace, Vol 8, Iss 9, p 248 (2021)
This paper treats a robust adaptive trajectory-tracking control design for a rotorcraft using a high-fidelity math model subject to model uncertainties. In order to control the nonlinear rotorcraft model which shows strong inter-axis coupling and hig
Externí odkaz:
https://doaj.org/article/ea9b9a97612f4009b045e64d8337b369
Publikováno v:
Aerospace, Vol 8, Iss 248, p 248 (2021)
Aerospace
Volume 8
Issue 9
Aerospace
Volume 8
Issue 9
This paper treats a robust adaptive trajectory-tracking control design for a rotorcraft using a high-fidelity math model subject to model uncertainties. In order to control the nonlinear rotorcraft model which shows strong inter-axis coupling and hig
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::50f6181f5f5f5065321b7b04bed9bbc1
https://www.mdpi.com/2226-4310/8/9/248
https://www.mdpi.com/2226-4310/8/9/248
Publikováno v:
International Journal of Aerospace Engineering, Vol 2021 (2021)
This paper investigates the adaptive incremental backstepping sliding mode control for the rotorcraft trajectory-tracking control problem to enhance the robustness to the matched uncertainty in the model. First, the incremental dynamics is used for t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8b33fee944a9dcd8dae4cd8ec990886a
Publikováno v:
Aerospace Science and Technology. 118:107014
Integrating multiple features for autonomous flight of aircraft requires extensive research over wide categories, high-level of know-how, and experiences. To contribute to these issues, this paper treats the realizable integration techniques of the p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2b0cf0d478df118c970ac1b983721cee
https://doi.org/10.1016/j.ast.2021.107014
https://doi.org/10.1016/j.ast.2021.107014