Adaptive terminal sliding mode control for hypersonic flight vehicles with strictly lower convex function based nonlinear disturbance observer-Reference-Cited by-同舟云学术

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Adaptive terminal sliding mode control for hypersonic flight vehicles with strictly lower convex function based nonlinear disturbance observer

Published:2017-11 Issue: Volume:71 Page:215-226
ISSN:0019-0578
Container-title:ISA Transactions
language:en
Short-container-title:ISA Transactions

Author:

Wu Yun-jie,Zuo Jing-xing,Sun Liang-hua

Publisher

Elsevier BV

Subject

Applied Mathematics,Control and Systems Engineering,Electrical and Electronic Engineering,Computer Science Applications,Instrumentation

Reference57 articles.

1. Recursive terminal sliding mode control for hypersonic flight vehicle with sliding mode disturbance observer;Wang;Nonlinear Dyn,2015

2. A review of design issues specific to hypersonic flight vehicles;Sziroczak;Prog Aerosp Sci,2016

3. Aeroservoelastic modeling and analysis of a six-DOF hypersonic flight vehicle;Zong;Proc Inst Mech Eng G J Aerosp,2016

4. Analysis of dynamic characteristics of the rigid body/elastic body coupling of air-breathing hypersonic vehicles;Zhang;Aerosp Sci Technol,2016

5. Modelling for couplings of an airframe-propulsion integrated hypersonic vehicle with engine safety boundaries;Yao;Proc Inst Mech Eng G J Aerosp,2010

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2. Finite-Time Dynamic Sliding Mode Control for Non-Minimum Phase Hypersonic Vehicle;2023 42nd Chinese Control Conference (CCC);2023-07-24

3. Adaptive Performance-Constrained Synchronization Control for Hypersonic Flight Vehicle Swarms: A Novel Finite-Time Convergence Protocol Methodology;Guidance, Navigation and Control;2023-06

4. Adaptive Sliding Mode Control with RBF Approximation for Hypersonic Flight Vehicle;Proceedings of 2022 International Conference on Autonomous Unmanned Systems (ICAUS 2022);2023

5. Distributed state estimator-based consensus tracking of multi-agent systems with exogenous disturbance;Journal of the Franklin Institute;2022-10

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