Prescribed performance-based low-computational cost fuzzy control of a hypersonic vehicle using non-affine models
Author:
Affiliation:
1. Air and Missile Defense College, Air Force Engineering University, Xi’an, China
2. School of Automation, Northwestern Polytechnical University, Xi’an, China
3. Air Force Engineering University, Xi’an, China
Publisher
SAGE Publications
Subject
Mechanical Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1177/1687814018757261
Reference34 articles.
1. Guaranteeing prescribed output tracking performance for air-breathing hypersonic vehicles via non-affine back-stepping control design
2. Adaptive Multivariable Integral TSMC of a Hypersonic Gliding Vehicle With Actuator Faults and Model Uncertainties
3. High-order tracking differentiator based adaptive neural control of a flexible air-breathing hypersonic vehicle subject to actuators constraints
4. A prescribed performance control approach guaranteeing small overshoot for air-breathing hypersonic vehicles via neural approximation
5. Flight-Test Experiment Design for Characterizing Stability and Control of Hypersonic Vehicles
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