Adaptive RBF Network-Based Sliding-Mode Fault-Tolerant Control for Hypersonic Vehicles With Model Uncertainties
Author:
Affiliation:
1. Beijing Institute of Technology,School of Automation,Beijing,China
2. Beijing Institute of Aerospace Technology,Beijing,China
3. Shanghai Institute of Aerospace Control Technology,Shanghai,China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx8/10587298/10587321/10587840.pdf?arnumber=10587840
Reference21 articles.
1. Flight-Propulsion Integration Dynamic Analysis and Adaptive Control of the Hypersonic Vehicle at Wide-Range Mach Numbers
2. Six-DOF Spacecraft Optimal Trajectory Planning and Real-Time Attitude Control: A Deep Neural Network-Based Approach
3. Self-Healing Control for Attitude System of Hypersonic Flight Vehicle With Body Flap Faults
4. Fractional-order proportional-integral-derivative linear active disturbance rejection control design and parameter optimization for hypersonic vehicles with actuator faults
5. Fault-Tolerant Attitude Control for Hypersonic Flight Vehicle Subject to Actuators Constraint: A Model Predictive Static Programming Approach
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