Attitude optimization control of hypersonic flight vehicle considering partially unknown control direction
Sign Up to like & getrecommendations! Published in 2022 at "Transactions of the Institute of Measurement and Control"
DOI: 10.1177/01423312221138124
Abstract: In this paper, a control method based on periodic sliding mode technology and adaptive dynamic programming algorithm is proposed for the attitude dynamics of hypersonic flight vehicle. The method takes into account a case that… read more here.
Keywords: control; hypersonic flight; control direction; unknown control ... See more keywords
Bifurcation analysis for a novel flight vehicle with pitch-control single moving mass
Sign Up to like & getrecommendations! Published in 2021 at "Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering"
DOI: 10.1177/09544100211023259
Abstract: Moving mass flight vehicle is a strongly nonlinear system under high speed flying conditions. The system attitude dynamics becomes even more complex due to the coupling between the internal moving mass with large mass ratio… read more here.
Keywords: flight vehicle; moving mass; bifurcation; mass ... See more keywords
Q-learning–based practical disturbance compensation control for hypersonic flight vehicle
Sign Up to like & getrecommendations! Published in 2022 at "Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering"
DOI: 10.1177/09544100221140242
Abstract: Aiming at the attitude control problem of hypersonic flight vehicle, a compound control strategy based on the disturbance compensation technique and Q-learning optimization is proposed. Firstly, a three-channel independent control scheme based on the super-twisting… read more here.
Keywords: disturbance; disturbance compensation; control; hypersonic flight ... See more keywords
Discrete reconfigurable back-stepping attitude control of reentry hypersonic flight vehicle
Sign Up to like & getrecommendations! Published in 2017 at "Advances in Mechanical Engineering"
DOI: 10.1177/1687814017703900
Abstract: A discrete reconfigurable back-stepping controller is proposed to resolve the attitude command tracking problem of hypersonic flight vehicle in reentry mode. The hypersonic flight vehicle dynamic equations are transformed into discrete form based on Euler… read more here.
Keywords: flight vehicle; back stepping; control; vehicle ... See more keywords