Zero-sum differential games-based fast adaptive robust optimal sliding mode control design for uncertain missile autopilot with constrained input
Author:
Affiliation:
1. College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, People's Republic of China
Funder
National Natural Science Foundation of China
Publisher
Informa UK Limited
Subject
Computer Science Applications,Control and Systems Engineering
Link
https://www.tandfonline.com/doi/pdf/10.1080/00207179.2021.1872802
Reference26 articles.
1. Disturbance suppression for quadrotor UAV using sliding-mode-observer-based equivalent-input-disturbance approach
2. Disturbance observer-based quadrotor attitude tracking control for aggressive maneuvers
3. Nonlinear Disturbance Observer-Enhanced Dynamic Inversion Control of Missiles
4. Adaptive Actor–Critic Design-Based Integral Sliding-Mode Control for Partially Unknown Nonlinear Systems With Input Disturbances
5. Three-dimensional terminal angle constrained robust guidance law with autopilot lag consideration
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