Constrained fault-tolerant control for hypersonic vehicle subject to actuator failure and with unmeasurable states
DOI10.1080/00207721.2021.1928327zbMath1483.93094OpenAlexW3186588393MaRDI QIDQ5029152
Ruiyun Qi, Daikun Chao, Bin Jiang
Publication date: 11 February 2022
Published in: International Journal of Systems Science (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1080/00207721.2021.1928327
fault-tolerant controlmultiple constraintshypersonic vehiclemodel predictive static programmingadaptive robust unscented Kalman filter
Filtering in stochastic control theory (93E11) Sensitivity (robustness) (93B35) Adaptive control/observation systems (93C40) Model predictive control (93B45)
Cites Work
- Unnamed Item
- A guaranteed transient performance-based adaptive neural control scheme with low-complexity computation for flexible air-breathing hypersonic vehicles
- Robust model predictive tracking control of hypersonic vehicles in the presence of actuator constraints and input delays
- Adaptive restricted trajectory tracking for a non-minimum phase hypersonic vehicle model
- Three-stage unscented Kalman filter for state and fault estimation of nonlinear system with unknown input
- Fault-tolerant anti-windup control for hypersonic vehicles in reentry based on ISMDO
- Multiple model predictive control for large envelope flight of hypersonic vehicle systems
- Nonlinear fuzzy fault-tolerant control of hypersonic flight vehicle with parametric uncertainty and actuator fault
- Adaptive fault-tolerance control based finite-time backstepping for hypersonic flight vehicle with full state constrains
- Performance evaluation of UKF-based nonlinear filtering
- A strong tracking extended Kalman observer for nonlinear discrete-time systems
- Data filtering-based parameter and state estimation algorithms for state-space systems disturbed by coloured noises
- Integrated methodology for state and parameter estimation of spark-ignition engines
This page was built for publication: Constrained fault-tolerant control for hypersonic vehicle subject to actuator failure and with unmeasurable states