Prescribed Performance Fault Tolerant Control for Hypersonic Flight Vehicles With Actuator Failures

This paper proposes a novel prescribed performance fault tolerant control for hypersonic flight vehicle nonaffine models with actuator failures. First, the hypersonic flight vehicle longitudinal model is decomposed into two subsystems: the altitude subsystem and the velocity subsystem, which are exp...

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Bibliographic Details
Main Authors: Siyuan Zhao, Xiaobing Li
Format: Article
Language:English
Published: IEEE 2019-01-01
Series:IEEE Access
Subjects:
Online Access:https://ieeexplore.ieee.org/document/8769975/