Attitude control of short-range loitering missile based on ADRC

DOI

10.2991/icmmcce-15.2015.140How to use a DOI?

Keywords

ADRC; Loitering Missile; Attitude Control

Abstract

ADRC (ADRC) has excellent control performance. The paper Introduces structure and discrete algorithms of the ADRC,and describes its parameter tuning rule. The ADRC control technology is applied to attitude control system design of short-range loitering missile, from the perspective of engineering applications, proposesing a design method of ADRC attitude controller, specifically addressing the principle of the method and process. Simulation results show that this method has strong robustness and adaptability, strong dynamic performance and stable performance.

Copyright

© 2015, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

Download article (PDF)

TY  - CONF
AU  - Rui Huang
AU  - Jianhui Chen
AU  - Ming Gao
AU  - Guiming Tao
PY  - 2015/12
DA  - 2015/12
TI  - Attitude control of short-range loitering missile based on ADRC
BT  - Proceedings of the 4th International Conference on Mechatronics, Materials, Chemistry and Computer Engineering 2015
PB  - Atlantis Press
SP  - 695
EP  - 699
SN  - 2352-538X
UR  - https://doi.org/10.2991/icmmcce-15.2015.140
DO  - 10.2991/icmmcce-15.2015.140
ID  - Huang2015/12
ER  -