Design of the Missile Attitude Controller Based on the Active Disturbance Rejection Control

Author:

Liu Shanzhong1ORCID,Xue Mengqi1ORCID,Qiu Yaolong1ORCID,Zhou Xingyu1ORCID,Zhao Qingxiu1ORCID

Affiliation:

1. Henan University of Science and Technology, China

Publisher

FapUNIFESP (SciELO)

Subject

Aerospace Engineering

Reference13 articles.

1. Disturbance observer based fuzzy PID and robust PID autopilot design for bank-to-turn missile;Basha SM,2017

2. PID control based missile sub-channel simulation;Chen CB;Adv Mater Res,2012

3. On the stability of linear active disturbance rejection control;Chen ZQ;Acta Autom Sin,2013

4. Scaling and bandwidth-parameterization based control tuning;Gao ZQ,2003

5. From PID technique to active disturbances rejection control technique;Han JQ;Control Engineering of China,2002

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4. A Novel Disturbance Rejection Control of Roll Channel for Small Air-to-Surface Missiles;Applied Sciences;2022-12-28

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