Tube-model predictive control based on sum of squares for hypersonic vehicle with state-dependent input constraints
Author:
Affiliation:
1. School of Electrical and Information Engineering, Tianjin University, China
2. Aviation Key Laboratory of Science and Technology on Aircraft Control, China
Abstract
Funder
Aeronautical Science Foundation of China
National Natural Science Foundation of China
Publisher
SAGE Publications
Subject
Instrumentation
Link
http://journals.sagepub.com/doi/pdf/10.1177/01423312211046504
Reference40 articles.
1. Anti-windup disturbance suppression control of feedback linearizable systems with application to hypersonic flight vehicles
2. Lectures on Modern Convex Optimization
3. Guaranteeing prescribed output tracking performance for air-breathing hypersonic vehicles via non-affine back-stepping control design
4. Tube-based robust MPC for linear time-varying systems with bounded disturbances
5. Feedforward and feedback linearization of nonlinear system and its implementation using internal model control (IMC)
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1. Preshaping Trajectory Optimization and Control of Flexible Hypersonic Vehicle for Vibration Suppression;2023 42nd Chinese Control Conference (CCC);2023-07-24
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