Trajectory based motion synchronization in a dissimilar redundant actuation system for a large civil aircraft

Waheed Ur Reliman; Haq Nawaz; Shaoping Wang; Xingjian Wang; Yuanxin Luo; Xu Yun; Muhammad Nadeem Iqbal; Mansoor Ali Zaheer; Irfan Azhar; Hassan Elahi

doi:10.1109/CCDC.2017.7979383

Trajectory based motion synchronization in a dissimilar redundant actuation system for a large civil aircraft

Waheed Ur Reliman
, Haq Nawaz
, Shaoping Wang
, Xingjian Wang
, Yuanxin Luo
, Xu Yun
, Muhammad Nadeem Iqbal
, Mansoor Ali Zaheer
, Irfan Azhar
, Hassan Elahi

School of Automation Science and Electrical Engineering

Chongqing University
Beihang University
Koc University
University of Rome La Sapienza

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

17 Scopus citations

Abstract

With the passage of time, the aircraft industry is moving towards more electric aircraft. This creates an opportunity to introduce dissimilar redundant actuation system in the primary flight control system. The problem arises, such as a force fighting (force difference between the outputs of actuators) in using dissimilar redundant actuation system. This paper presents a strategy to reduce force fighting for redundant actuation system of hydraulic actuator (HA) and electro hydrostatic actuator (EHA). A trajectory is designed on the basis of dynamic characteristics of the EHA. The feedback controller is used to improve load rejection performance and the two feed forward controllers to remove the initial force fighting between HA and EHA.

Original language	English
Title of host publication	Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	5010-5015
Number of pages	6
ISBN (Electronic)	9781509046560
DOIs	https://doi.org/10.1109/CCDC.2017.7979383
State	Published - 12 Jul 2017
Event	29th Chinese Control and Decision Conference, CCDC 2017 - Chongqing, China Duration: 28 May 2017 → 30 May 2017

Publication series

Name	Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017

Conference

Conference	29th Chinese Control and Decision Conference, CCDC 2017
Country/Territory	China
City	Chongqing
Period	28/05/17 → 30/05/17

Keywords

Feedback control
Feedforward Control
Redundant actuation system
Synchronous control
Tracking
Trajectory motion

Access to Document

10.1109/CCDC.2017.7979383

Cite this

Reliman, W. U., Nawaz, H., Wang, S., Wang, X., Luo, Y., Yun, X., Iqbal, M. N., Zaheer, M. A., Azhar, I., & Elahi, H. (2017). Trajectory based motion synchronization in a dissimilar redundant actuation system for a large civil aircraft. In Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017 (pp. 5010-5015). Article 7979383 (Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CCDC.2017.7979383

Reliman, Waheed Ur ; Nawaz, Haq ; Wang, Shaoping et al. / Trajectory based motion synchronization in a dissimilar redundant actuation system for a large civil aircraft. Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017. Institute of Electrical and Electronics Engineers Inc., 2017. pp. 5010-5015 (Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017).

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title = "Trajectory based motion synchronization in a dissimilar redundant actuation system for a large civil aircraft",

abstract = "With the passage of time, the aircraft industry is moving towards more electric aircraft. This creates an opportunity to introduce dissimilar redundant actuation system in the primary flight control system. The problem arises, such as a force fighting (force difference between the outputs of actuators) in using dissimilar redundant actuation system. This paper presents a strategy to reduce force fighting for redundant actuation system of hydraulic actuator (HA) and electro hydrostatic actuator (EHA). A trajectory is designed on the basis of dynamic characteristics of the EHA. The feedback controller is used to improve load rejection performance and the two feed forward controllers to remove the initial force fighting between HA and EHA.",

keywords = "Feedback control, Feedforward Control, Redundant actuation system, Synchronous control, Tracking, Trajectory motion",

author = "Reliman, \{Waheed Ur\} and Haq Nawaz and Shaoping Wang and Xingjian Wang and Yuanxin Luo and Xu Yun and Iqbal, \{Muhammad Nadeem\} and Zaheer, \{Mansoor Ali\} and Irfan Azhar and Hassan Elahi",

note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 29th Chinese Control and Decision Conference, CCDC 2017 ; Conference date: 28-05-2017 Through 30-05-2017",

year = "2017",

month = jul,

day = "12",

doi = "10.1109/CCDC.2017.7979383",

language = "英语",

series = "Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017",

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Reliman, WU, Nawaz, H, Wang, S , Wang, X, Luo, Y, Yun, X, Iqbal, MN, Zaheer, MA, Azhar, I & Elahi, H 2017, Trajectory based motion synchronization in a dissimilar redundant actuation system for a large civil aircraft. in Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017., 7979383, Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017, Institute of Electrical and Electronics Engineers Inc., pp. 5010-5015, 29th Chinese Control and Decision Conference, CCDC 2017, Chongqing, China, 28/05/17. https://doi.org/10.1109/CCDC.2017.7979383

Trajectory based motion synchronization in a dissimilar redundant actuation system for a large civil aircraft. / Reliman, Waheed Ur; Nawaz, Haq; Wang, Shaoping et al.
Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017. Institute of Electrical and Electronics Engineers Inc., 2017. p. 5010-5015 7979383 (Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017).

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

TY - GEN

T1 - Trajectory based motion synchronization in a dissimilar redundant actuation system for a large civil aircraft

AU - Reliman, Waheed Ur

AU - Nawaz, Haq

AU - Wang, Shaoping

AU - Wang, Xingjian

AU - Luo, Yuanxin

AU - Yun, Xu

AU - Iqbal, Muhammad Nadeem

AU - Zaheer, Mansoor Ali

AU - Azhar, Irfan

AU - Elahi, Hassan

PY - 2017/7/12

Y1 - 2017/7/12

N2 - With the passage of time, the aircraft industry is moving towards more electric aircraft. This creates an opportunity to introduce dissimilar redundant actuation system in the primary flight control system. The problem arises, such as a force fighting (force difference between the outputs of actuators) in using dissimilar redundant actuation system. This paper presents a strategy to reduce force fighting for redundant actuation system of hydraulic actuator (HA) and electro hydrostatic actuator (EHA). A trajectory is designed on the basis of dynamic characteristics of the EHA. The feedback controller is used to improve load rejection performance and the two feed forward controllers to remove the initial force fighting between HA and EHA.

AB - With the passage of time, the aircraft industry is moving towards more electric aircraft. This creates an opportunity to introduce dissimilar redundant actuation system in the primary flight control system. The problem arises, such as a force fighting (force difference between the outputs of actuators) in using dissimilar redundant actuation system. This paper presents a strategy to reduce force fighting for redundant actuation system of hydraulic actuator (HA) and electro hydrostatic actuator (EHA). A trajectory is designed on the basis of dynamic characteristics of the EHA. The feedback controller is used to improve load rejection performance and the two feed forward controllers to remove the initial force fighting between HA and EHA.

KW - Feedback control

KW - Feedforward Control

KW - Redundant actuation system

KW - Synchronous control

KW - Tracking

KW - Trajectory motion

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ER -

Reliman WU, Nawaz H, Wang S , Wang X, Luo Y, Yun X et al. Trajectory based motion synchronization in a dissimilar redundant actuation system for a large civil aircraft. In Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017. Institute of Electrical and Electronics Engineers Inc. 2017. p. 5010-5015. 7979383. (Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017). doi: 10.1109/CCDC.2017.7979383

Trajectory based motion synchronization in a dissimilar redundant actuation system for a large civil aircraft

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Keywords

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