Large-angle and High-speed Trajectory Tracking Control of a Quadrotor UAV based on Reachability
Author:
Affiliation:
1. The Hong Kong University of Science and Technology,Department of Mechanical and Aerospace En-gineering,Hong Kong,China
2. The Hong Kong University of Science and Technology,Department of Mechanical and Aerospace Engineering,Hong Kong,China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9811522/9811357/09811879.pdf?arnumber=9811879
Reference17 articles.
1. Switching control of attitude tracking on a quadrotor UAV for large-angle rotational maneuvers
2. Disturbance observer-based quadrotor attitude tracking control for aggressive maneuvers
3. Minimum snap trajectory generation and control for quadrotors
4. A geometric interpretation of pontryagin's maximum principle1;roxin;International Symposium on Nonlinear Differential Equations and Nonlinear Mechanics,0
5. Realization of Reachability for the Control of a Class of Nonlinear Systems
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1. Inverse dynamics based aerodynamic, gyroscopic, and rotor effects’ compensation in constrained trajectory synthesis for multi-copters;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2024-04-02
2. Simultaneous Planning and Execution for Quadrotors Flying Through a Narrow Gap Under Disturbance;IEEE Transactions on Control Systems Technology;2023-11
3. Simultaneous Planning and Execution for Safe Flight of Quadrotors suffering One Rotor Loss and Disturbance;IEEE Transactions on Aerospace and Electronic Systems;2023
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