Proceedings of the 4th International Conference on Mechatronics, Materials, Chemistry and Computer Engineering 2015

Attitude control of short-range loitering missile based on ADRC

Authors
Rui Huang, Jianhui Chen, Ming Gao, Guiming Tao
Corresponding Author
Rui Huang
Available Online December 2015.
DOI
https://doi.org/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.
Open Access
This is an open access article distributed under the CC BY-NC license.

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Cite this article

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  - https://doi.org/10.2991/icmmcce-15.2015.140
ID  - Huang2015/12
ER  -