Design of Lateral Three-Loop Autopilot with Pseudo-Angle of Sideslip Feedback Based on Active Disturbance Rejection Control

Author:

Wang Heting1,Wang Hui1,Guo Keqing1,Tang Daoguang2,Lei Yuanyue1

Affiliation:

1. School of Aerospace Engineering, Beijing Institute of Technology,Beijing,China,100081

2. School of Electrical and Control Engineering, North University of china,Taiyuan,China,030051

Publisher

IEEE

Reference20 articles.

1. The application of active disturbance rejection controller to estimating maneuvering target states for tank;qiu;Acta Armamentarii,2009

2. Active disturbance rejection control for uncertain time-delay nonlinear systems;ran;Automatica,2020

3. Command filtered back stepping guidance law considering autopilot dynamics;liu;Acta Aeronautica et Astronautica Sinica,2020

4. Scaling and bandwidth-parameterization based controller tuning;gao;Proceedings of the 2003 American Control Conference,2003

5. How autopilot requirements constrain the aerodynamic design of homing missiles;william nesline;American Control Conference San Diego,0

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