Nonlinear Robust Adaptive Deterministic Control for Flexible Hypersonic Vehicles in the Presence of Input Constraint-Reference-Cited by-同舟云学术

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Nonlinear Robust Adaptive Deterministic Control for Flexible Hypersonic Vehicles in the Presence of Input Constraint

Published:2015-05-13 Issue:6 Volume:17 Page:2303-2316
ISSN:1561-8625
Container-title:Asian Journal of Control
language:en
Short-container-title:Asian Journal of Control

Author:

Tian Bailing,Fan Wenru,Su Rui,Zong Qun

Funder

National Natural Science Foundation of China

Tianjin Research Program of Application Foundation and Advanced Technology

Aeronautical Science Foundation of China

Science and Technology on Aircraft Control Laboratory, and Independent Innovation Fund of Tianjin University

Publisher

Wiley

Subject

Control and Systems Engineering

Reference36 articles.

1. Robust fault-tolerant control of launch vehicle via GPI observer and integral sliding mode control;Zhao;Asian J. Control,2013

2. Adaptive dynamic surface control of a hypersonic flight vehicle with improved tracking;Butt;Asian J. Control,2013

3. Williams , T. M. A. Bolender D. B. Doman et al An aero-thermal flexible model analysis of a hypersonic vehicle AIAA Atmos. Flight Mech. Conf. 2006

4. Sigthorsson , D. O. A. Serrani Development of linear parameter-varying models of hypersonic air-breathing vehicles AIAA Guid. Nav. Contr. Conf 2009

5. Nonlinear longitudinal dynamical model of an air-breathing hypersonic vehicle;Bolender;J. Spacecr. Rockets,2007

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