Nonsingular Terminal Sliding Mode Control-based Prescribed Performance Guidance Law with Impact Angle Constraints

Conventional guidance law designs can only guarantee steady-state performance. However, transient performance is also the key performance index in practical guidance applications. In this paper, a novel terminal guidance law is presented for missile intercepting maneuvering target with impact angle...

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Veröffentlicht in:	International journal of control, automation, and systems Jg. 20; H. 3; S. 715 - 726
Hauptverfasser:	Ming, Chao, Wang, Xiaoming
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Bucheon / Seoul Institute of Control, Robotics and Systems and The Korean Institute of Electrical Engineers 01.03.2022 Springer Nature B.V 제어·로봇·시스템학회
Schlagworte:	Control Engineering Feedback control Guidance (motion) Impact angle Interception Maneuvering targets Mechatronics Performance indices Regular Papers Robotics Sliding mode control State observers Steady state Systems stability Terminal guidance Tracking control Tracking errors Transient performance 제어계측공학 impact angle Extended state observer terminal guidance law prescribed performance control nonsingular terminal sliding mode control
ISSN:	1598-6446, 2005-4092
Online-Zugang:	Volltext
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