Fault-Tolerant Attitude Control for Hypersonic Flight Vehicle Subject to Actuators Constraint: A Model Predictive Static Programming Approach
Author:
Affiliation:
1. Department of Control Theory and Control Engineering, School of Automation, Northwestern Polytechnical University, Xi’an, China
Funder
National Natural Science Foundation of China
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Pharmacology (medical)
Link
http://xplorestaging.ieee.org/ielx7/8253411/10131919/10034744.pdf?arnumber=10034744
Reference32 articles.
1. A new adaptive neural control scheme for hypersonic vehicle with actuators multiple constraints
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4. Model predictive control of hypersonic vehicles accommodating constraints
5. Generalized model predictive static programming and angle-constrained guidance of air-to-ground missiles;padhi;J Guid Control Dyn,2014
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