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contributor authorZihao Wu
contributor authorXiwang Dong
contributor authorQingdong Li
contributor authorJianglong Yu
contributor authorDaikai Liu
date accessioned2024-04-27T22:39:24Z
date available2024-04-27T22:39:24Z
date issued2024/01/01
identifier other10.1061-JAEEEZ.ASENG-5049.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4297181
description abstractIn this paper, a prescribed-time guidance law with approach angle constraint in the presence of an actuator fault is proposed. Firstly, a sliding mode manifold with prescribed-time convergence is given to ensure that the state of the system converges to the equilibrium point in the specified time. Then, in order to suppress the distrubance, an adaptive gain based on adaptive control is designed. Subsequntly, a augmentation term based on the Lyapunov method is presented to meet the prescribed-time convergence prpoperty when an actuator fault occurs. The prescribed-time convergence of the proposed guidance laws is proven. Numerical simulation results validate the effectiveness of the proposed prescribed-time guidance framework.
publisherASCE
titlePrescribed-Time Guidance Law with Approach Angle Constraint and Actuator Faults
typeJournal Article
journal volume37
journal issue1
journal titleJournal of Aerospace Engineering
identifier doi10.1061/JAEEEZ.ASENG-5049
journal fristpage04023107-1
journal lastpage04023107-11
page11
treeJournal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 001
contenttypeFulltext


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