The Design of Quadrotor UAV Based on Nonlinear Active Disturbance Rejection Control
Author:
Affiliation:
1. Tianjin University of Technology,College of Electrical and Electronic Engineering,Tianjin,China
2. Tianjin Labor Security Technician College,Department of Mechanical and Electrical Engineering,Tianjin,China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx8/10587298/10587321/10588175.pdf?arnumber=10588175
Reference19 articles.
1. Robust trajectory tracking control for a quadrotor using recursive sliding mode control and nonlinear extended state observer
2. PID control of quadrotor UAVs: A survey
3. Robust LQR and LQR-PI control strategies based on adaptive weighting matrix selection for a UAV position and attitude tracking control
4. An integral predictive/nonlinear H∞ control structure for a quadrotor helicopter
5. Nonsingular terminal sliding mode control for a quadrotor UAV with a total rotor failure
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