Modelling and Analysis About a Fault State of a New Cockpit Control Mechanism

Jingru Wang; Sen Liang

doi:doi:10.11648/j.ajae.20190601.13

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Modelling and Analysis About a Fault State of a New Cockpit Control Mechanism

Jingru Wang, Sen Liang

Published in American Journal of Aerospace Engineering (Volume 6, Issue 1)

Received: 17 July 2019 Accepted: 19 August 2019 Published: 4 September 2019

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Abstract

In the process of aircraft development, the assessment of handling quality is particularly step for verifying the cockpit control units design whether meets the design requirements or not. If the assess results are not met the design requirements, the design must to be optimized or even redesigned. At present, most of research is mainly related to the design of cockpit control units and simulating and assessment of their maneuverability based on the dynamic model in the normal mode, however, the research on handling quality of cockpit control units in the failure operating mode is seldom. Moreover, override rod linkage form as a new kind of cockpit control units brings plenty of profits such as the weight saved and maintainability improved, however, it causes the failure mode becomes diverse and complicated. Therefore it will increase the difficulty of assessing this kind of cockpit control units. The object of this paper is to do a research on working principle and physical characteristics of cockpit control units of override rod linkage form, through modeling and simulation on its normal operating mode and failure mode, and finally gives an analysis and evaluation for the column force quality of each failure mode. The simulation results reveal the column force quality of each failure mode is acceptable.

Published in	American Journal of Aerospace Engineering (Volume 6, Issue 1)
DOI	10.11648/j.ajae.20190601.13
Page(s)	17-23
Creative Commons	This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited.
Copyright	Copyright © The Author(s), 2024. Published by Science Publishing Group

Keywords

Fly-By-Wire Civil Aircraft, Cockpit Control Units, Override Rod, Failure Mode, Flight Quality Evaluation

References

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[4]	Zheng Shutao, Liao Feng, Wang Liwen. Experimental Study of Control Loading System of the Flight Simulator [J]. Journal of System Simulation, 2008, 20 (4): 965-969.
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[7]	Tian Jinqiang, Xue Ying, Guo Jianwei. The Kinetics Simulation of Fly-by-Wire Aircraft Control Column System [J]. Civil Aircraft Design and Research Institute, 2012, 25 (3): 53-56.
[8]	Zhang Yusong. Study on Control Loading System in Flight Simulator Base on the Electro-Motive [D]. Tianjin: Civil Aviation University of China, 2009.
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[10]	Wang Junlong. Research on Mechanism Structure and Control Scheme of Active Side-stick in Aeroplane [D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2008
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[12]	Zhang Fang, The Operating Components in Cockpit of Fly-by-Wire Flight Control System Research [J]. Beijing: China Aeronautical academy, 2014.
[13]	Lin Fengjun. Design and analysis of CRJ200 aircraft flight control system [J]. Shanghai: Design and research of civil aircraft, 2001, 4, 32-39.
[14]	Ding Zuoquan. Active Side-stick Control System for Aeroplane [D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2011.
[15]	Gao Jinyuan, Li Luyu, Feng Yachang. Aircraft Handing Qualities [M]. Beijing: National Defence Industry Press, 2003: 31-47.
[16]	Tom Berger and Mark B. Handling Qualities Flight Test Assessment of a Business Jet NzU P-β Fly-By-Wire Control System [J]. American Institute of Aeronautics and Astronautics, 2017.
[17]	Berger, T., Tischler, M. B., Hagerott, S. G., Cotting, M. C., Gresham, J. L., George, J. E., Krogh, K. J., D’Argenio, A., and Howland, J. D., “Development and Validation of a Flight Identiﬁed Business Jet Simulation Model Using a Stitching Architecture,” AIAA Modeling and Simulation Technologies Conference, Grapevine, TX, January 2017.

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APA Style

Jingru Wang, Sen Liang. (2019). Modelling and Analysis About a Fault State of a New Cockpit Control Mechanism. American Journal of Aerospace Engineering, 6(1), 17-23. https://doi.org/10.11648/j.ajae.20190601.13

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ACS Style

Jingru Wang; Sen Liang. Modelling and Analysis About a Fault State of a New Cockpit Control Mechanism. Am. J. Aerosp. Eng. 2019, 6(1), 17-23. doi: 10.11648/j.ajae.20190601.13

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AMA Style

Jingru Wang, Sen Liang. Modelling and Analysis About a Fault State of a New Cockpit Control Mechanism. Am J Aerosp Eng. 2019;6(1):17-23. doi: 10.11648/j.ajae.20190601.13

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@article{10.11648/j.ajae.20190601.13,
  author = {Jingru Wang and Sen Liang},
  title = {Modelling and Analysis About a Fault State of a New Cockpit Control Mechanism},
  journal = {American Journal of Aerospace Engineering},
  volume = {6},
  number = {1},
  pages = {17-23},
  doi = {10.11648/j.ajae.20190601.13},
  url = {https://doi.org/10.11648/j.ajae.20190601.13},
  eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.ajae.20190601.13},
  abstract = {In the process of aircraft development, the assessment of handling quality is particularly step for verifying the cockpit control units design whether meets the design requirements or not. If the assess results are not met the design requirements, the design must to be optimized or even redesigned. At present, most of research is mainly related to the design of cockpit control units and simulating and assessment of their maneuverability based on the dynamic model in the normal mode, however, the research on handling quality of cockpit control units in the failure operating mode is seldom. Moreover, override rod linkage form as a new kind of cockpit control units brings plenty of profits such as the weight saved and maintainability improved, however, it causes the failure mode becomes diverse and complicated. Therefore it will increase the difficulty of assessing this kind of cockpit control units. The object of this paper is to do a research on working principle and physical characteristics of cockpit control units of override rod linkage form, through modeling and simulation on its normal operating mode and failure mode, and finally gives an analysis and evaluation for the column force quality of each failure mode. The simulation results reveal the column force quality of each failure mode is acceptable.},
 year = {2019}
}

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TY  - JOUR
T1  - Modelling and Analysis About a Fault State of a New Cockpit Control Mechanism
AU  - Jingru Wang
AU  - Sen Liang
Y1  - 2019/09/04
PY  - 2019
N1  - https://doi.org/10.11648/j.ajae.20190601.13
DO  - 10.11648/j.ajae.20190601.13
T2  - American Journal of Aerospace Engineering
JF  - American Journal of Aerospace Engineering
JO  - American Journal of Aerospace Engineering
SP  - 17
EP  - 23
PB  - Science Publishing Group
SN  - 2376-4821
UR  - https://doi.org/10.11648/j.ajae.20190601.13
AB  - In the process of aircraft development, the assessment of handling quality is particularly step for verifying the cockpit control units design whether meets the design requirements or not. If the assess results are not met the design requirements, the design must to be optimized or even redesigned. At present, most of research is mainly related to the design of cockpit control units and simulating and assessment of their maneuverability based on the dynamic model in the normal mode, however, the research on handling quality of cockpit control units in the failure operating mode is seldom. Moreover, override rod linkage form as a new kind of cockpit control units brings plenty of profits such as the weight saved and maintainability improved, however, it causes the failure mode becomes diverse and complicated. Therefore it will increase the difficulty of assessing this kind of cockpit control units. The object of this paper is to do a research on working principle and physical characteristics of cockpit control units of override rod linkage form, through modeling and simulation on its normal operating mode and failure mode, and finally gives an analysis and evaluation for the column force quality of each failure mode. The simulation results reveal the column force quality of each failure mode is acceptable.
VL  - 6
IS  - 1
ER  -

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Author Information

Jingru Wang

Flight Control Department, AVIC XAC Commercial Aircraft CO., LTD, Xi'an City, China
Sen Liang

Flight Control Department, AVIC XAC Commercial Aircraft CO., LTD, Xi'an City, China; Flight Control Department, First Aircraft Design Institute, Xi'an City, China

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Plain Text BibTeX RIS

APA Style

Jingru Wang, Sen Liang. (2019). Modelling and Analysis About a Fault State of a New Cockpit Control Mechanism. American Journal of Aerospace Engineering, 6(1), 17-23. https://doi.org/10.11648/j.ajae.20190601.13

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ACS Style

Jingru Wang; Sen Liang. Modelling and Analysis About a Fault State of a New Cockpit Control Mechanism. Am. J. Aerosp. Eng. 2019, 6(1), 17-23. doi: 10.11648/j.ajae.20190601.13

Copy | Download

AMA Style

Jingru Wang, Sen Liang. Modelling and Analysis About a Fault State of a New Cockpit Control Mechanism. Am J Aerosp Eng. 2019;6(1):17-23. doi: 10.11648/j.ajae.20190601.13

Copy | Download

@article{10.11648/j.ajae.20190601.13,
  author = {Jingru Wang and Sen Liang},
  title = {Modelling and Analysis About a Fault State of a New Cockpit Control Mechanism},
  journal = {American Journal of Aerospace Engineering},
  volume = {6},
  number = {1},
  pages = {17-23},
  doi = {10.11648/j.ajae.20190601.13},
  url = {https://doi.org/10.11648/j.ajae.20190601.13},
  eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.ajae.20190601.13},
  abstract = {In the process of aircraft development, the assessment of handling quality is particularly step for verifying the cockpit control units design whether meets the design requirements or not. If the assess results are not met the design requirements, the design must to be optimized or even redesigned. At present, most of research is mainly related to the design of cockpit control units and simulating and assessment of their maneuverability based on the dynamic model in the normal mode, however, the research on handling quality of cockpit control units in the failure operating mode is seldom. Moreover, override rod linkage form as a new kind of cockpit control units brings plenty of profits such as the weight saved and maintainability improved, however, it causes the failure mode becomes diverse and complicated. Therefore it will increase the difficulty of assessing this kind of cockpit control units. The object of this paper is to do a research on working principle and physical characteristics of cockpit control units of override rod linkage form, through modeling and simulation on its normal operating mode and failure mode, and finally gives an analysis and evaluation for the column force quality of each failure mode. The simulation results reveal the column force quality of each failure mode is acceptable.},
 year = {2019}
}

Copy | Download

TY  - JOUR
T1  - Modelling and Analysis About a Fault State of a New Cockpit Control Mechanism
AU  - Jingru Wang
AU  - Sen Liang
Y1  - 2019/09/04
PY  - 2019
N1  - https://doi.org/10.11648/j.ajae.20190601.13
DO  - 10.11648/j.ajae.20190601.13
T2  - American Journal of Aerospace Engineering
JF  - American Journal of Aerospace Engineering
JO  - American Journal of Aerospace Engineering
SP  - 17
EP  - 23
PB  - Science Publishing Group
SN  - 2376-4821
UR  - https://doi.org/10.11648/j.ajae.20190601.13
AB  - In the process of aircraft development, the assessment of handling quality is particularly step for verifying the cockpit control units design whether meets the design requirements or not. If the assess results are not met the design requirements, the design must to be optimized or even redesigned. At present, most of research is mainly related to the design of cockpit control units and simulating and assessment of their maneuverability based on the dynamic model in the normal mode, however, the research on handling quality of cockpit control units in the failure operating mode is seldom. Moreover, override rod linkage form as a new kind of cockpit control units brings plenty of profits such as the weight saved and maintainability improved, however, it causes the failure mode becomes diverse and complicated. Therefore it will increase the difficulty of assessing this kind of cockpit control units. The object of this paper is to do a research on working principle and physical characteristics of cockpit control units of override rod linkage form, through modeling and simulation on its normal operating mode and failure mode, and finally gives an analysis and evaluation for the column force quality of each failure mode. The simulation results reveal the column force quality of each failure mode is acceptable.
VL  - 6
IS  - 1
ER  -

Copy | Download