Lateral thrust and aerodynamics blended control system design based on auto disturbance-rejection controller

Yuhang Wang; Yu Yao; Kemao Ma

doi:10.1109/ICAL.2008.4636187

Lateral thrust and aerodynamics blended control system design based on auto disturbance-rejection controller

Yuhang Wang^*
, Yu Yao
, Kemao Ma

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

8 Scopus citations

Abstract

Auto disturbance-rejection controller technique is applied to the synthesis of a longitudinal autopilot for a missile with lateral thrust and aerodynamics blended. At first, the characteristics and the main control problem for blended system are analyzed and the blended control model is established. Then, three close loops design method is proposed for the blended control system. The inner-loop and medium-loop are designed by auto disturbance-rejection controller, which is insensitive to the variation of the plant parameters and external disturbance. The external-loop is designed by PI controller. The simulation results show that the designed system attains high dynamic performance and steady-state performance and the controller has excellent robustness performance.

Original language	English
Title of host publication	Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2008
Pages	416-420
Number of pages	5
DOIs	https://doi.org/10.1109/ICAL.2008.4636187
State	Published - 2008
Event	IEEE International Conference on Automation and Logistics, ICAL 2008 - Qingdao, China Duration: 1 Sep 2008 → 3 Sep 2008

Publication series

Name	Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2008

Conference

Conference	IEEE International Conference on Automation and Logistics, ICAL 2008
Country/Territory	China
City	Qingdao
Period	1/09/08 → 3/09/08

Keywords

Auto disturbance-rejection controller (ADRC)
Blended control system
Interception missile
Lateral thrust

Access to Document

10.1109/ICAL.2008.4636187

Cite this

Wang, Y., Yao, Y., & Ma, K. (2008). Lateral thrust and aerodynamics blended control system design based on auto disturbance-rejection controller. In Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2008 (pp. 416-420). Article 4636187 (Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2008). https://doi.org/10.1109/ICAL.2008.4636187

@inproceedings{0b65895e6e7c4419b996d4e6c05fbe79,

title = "Lateral thrust and aerodynamics blended control system design based on auto disturbance-rejection controller",

abstract = "Auto disturbance-rejection controller technique is applied to the synthesis of a longitudinal autopilot for a missile with lateral thrust and aerodynamics blended. At first, the characteristics and the main control problem for blended system are analyzed and the blended control model is established. Then, three close loops design method is proposed for the blended control system. The inner-loop and medium-loop are designed by auto disturbance-rejection controller, which is insensitive to the variation of the plant parameters and external disturbance. The external-loop is designed by PI controller. The simulation results show that the designed system attains high dynamic performance and steady-state performance and the controller has excellent robustness performance.",

keywords = "Auto disturbance-rejection controller (ADRC), Blended control system, Interception missile, Lateral thrust",

author = "Yuhang Wang and Yu Yao and Kemao Ma",

year = "2008",

doi = "10.1109/ICAL.2008.4636187",

language = "英语",

isbn = "9781424425020",

series = "Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2008",

pages = "416--420",

booktitle = "Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2008",

note = "IEEE International Conference on Automation and Logistics, ICAL 2008 ; Conference date: 01-09-2008 Through 03-09-2008",

}

Wang, Y, Yao, Y & Ma, K 2008, Lateral thrust and aerodynamics blended control system design based on auto disturbance-rejection controller. in Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2008., 4636187, Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2008, pp. 416-420, IEEE International Conference on Automation and Logistics, ICAL 2008, Qingdao, China, 1/09/08. https://doi.org/10.1109/ICAL.2008.4636187

Lateral thrust and aerodynamics blended control system design based on auto disturbance-rejection controller. / Wang, Yuhang; Yao, Yu; Ma, Kemao.
Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2008. 2008. p. 416-420 4636187 (Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2008).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Lateral thrust and aerodynamics blended control system design based on auto disturbance-rejection controller

AU - Wang, Yuhang

AU - Yao, Yu

AU - Ma, Kemao

PY - 2008

Y1 - 2008

N2 - Auto disturbance-rejection controller technique is applied to the synthesis of a longitudinal autopilot for a missile with lateral thrust and aerodynamics blended. At first, the characteristics and the main control problem for blended system are analyzed and the blended control model is established. Then, three close loops design method is proposed for the blended control system. The inner-loop and medium-loop are designed by auto disturbance-rejection controller, which is insensitive to the variation of the plant parameters and external disturbance. The external-loop is designed by PI controller. The simulation results show that the designed system attains high dynamic performance and steady-state performance and the controller has excellent robustness performance.

AB - Auto disturbance-rejection controller technique is applied to the synthesis of a longitudinal autopilot for a missile with lateral thrust and aerodynamics blended. At first, the characteristics and the main control problem for blended system are analyzed and the blended control model is established. Then, three close loops design method is proposed for the blended control system. The inner-loop and medium-loop are designed by auto disturbance-rejection controller, which is insensitive to the variation of the plant parameters and external disturbance. The external-loop is designed by PI controller. The simulation results show that the designed system attains high dynamic performance and steady-state performance and the controller has excellent robustness performance.

KW - Auto disturbance-rejection controller (ADRC)

KW - Blended control system

KW - Interception missile

KW - Lateral thrust

UR - https://www.scopus.com/pages/publications/56449116922

U2 - 10.1109/ICAL.2008.4636187

DO - 10.1109/ICAL.2008.4636187

M3 - 会议稿件

AN - SCOPUS:56449116922

SN - 9781424425020

T3 - Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2008

SP - 416

EP - 420

BT - Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2008

T2 - IEEE International Conference on Automation and Logistics, ICAL 2008

Y2 - 1 September 2008 through 3 September 2008

ER -

Wang Y, Yao Y, Ma K. Lateral thrust and aerodynamics blended control system design based on auto disturbance-rejection controller. In Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2008. 2008. p. 416-420. 4636187. (Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2008). doi: 10.1109/ICAL.2008.4636187

Lateral thrust and aerodynamics blended control system design based on auto disturbance-rejection controller

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