2021
DOI: 10.1108/aeat-11-2020-0253
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Predefined-time control for a horizontal takeoff and horizontal landing reusable launch vehicle

Abstract: Purpose This paper aims to investigate the problem of attitude control for a horizontal takeoff and horizontal landing reusable launch vehicle. Design/methodology/approach In this paper, a predefined-time attitude tracking controller is presented for a horizontal takeoff and horizontal landing reusable launch vehicle (HTHLRLV). Firstly, the attitude tracking error dynamics model of the HTHLRLV is developed. Subsequently, a novel sliding mode surface is designed with predefined-time stability. Furthermore, by… Show more

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Cited by 8 publications
(2 citation statements)
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“…proof Under the action of the control law u, the sliding surface reaches a stable point, that is, S = 0 [24] . We can get…”
Section: Appointed Time Controller Designmentioning
confidence: 97%
“…proof Under the action of the control law u, the sliding surface reaches a stable point, that is, S = 0 [24] . We can get…”
Section: Appointed Time Controller Designmentioning
confidence: 97%
“…The control action will switch to the secondary Controller II when the libration disturbance appears. The Controller II suppresses the libration to zero within one time step of the Controller I by a novel prescribed-time control (PTC) law based on the fixed-time control scheme [28][29][30]. The stability of the proposed control strategy is proved under the Lyapunov framework.…”
Section: Introductionmentioning
confidence: 99%