Design of flight control system for a Hypersonic Gliding Vehicle based on nonlinear disturbance observer

Chengshan Qian; Changyin Sun; Yiqing Huang; Chaoxu Mu; Jingmei Zhang; Ruimin Zhang

doi:10.1109/ICCA.2013.6564958

Design of flight control system for a Hypersonic Gliding Vehicle based on nonlinear disturbance observer

Chengshan Qian
, Changyin Sun
, Yiqing Huang
, Chaoxu Mu
, Jingmei Zhang
, Ruimin Zhang

Southeast University, Nanjing

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

12 Scopus citations

Abstract

Hypersonic Gliding Vehicle (HGV) is a new class of hypersonic glider being developed. This paper designs a flight control system for a Hypersonic Gliding Vehicle based on nonlinear disturbance observers. Firstly, a nonlinear disturbance observer (NDO) is used to estimate the unknown disturbances; the influence of disturbances is estimated by the NDO. Secondly, the NDO is integrated with a conventional sliding mode controller to compensate the influence of disturbances based on the estimate. Stability of the composite closed-loop system is provided using Lyapunov theory. Finally, simulation results present that the flight control system for the HGV achieves excellent results.

Original language	English
Title of host publication	2013 10th IEEE International Conference on Control and Automation, ICCA 2013
Pages	1573-1577
Number of pages	5
DOIs	https://doi.org/10.1109/ICCA.2013.6564958
State	Published - 2013
Externally published	Yes
Event	2013 10th IEEE International Conference on Control and Automation, ICCA 2013 - Hangzhou, China Duration: 12 Jun 2013 → 14 Jun 2013

Publication series

Name	IEEE International Conference on Control and Automation, ICCA
ISSN (Print)	1948-3449
ISSN (Electronic)	1948-3457

Conference

Conference	2013 10th IEEE International Conference on Control and Automation, ICCA 2013
Country/Territory	China
City	Hangzhou
Period	12/06/13 → 14/06/13

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10.1109/ICCA.2013.6564958

Cite this

Qian, C., Sun, C., Huang, Y., Mu, C., Zhang, J., & Zhang, R. (2013). Design of flight control system for a Hypersonic Gliding Vehicle based on nonlinear disturbance observer. In 2013 10th IEEE International Conference on Control and Automation, ICCA 2013 (pp. 1573-1577). Article 6564958 (IEEE International Conference on Control and Automation, ICCA). https://doi.org/10.1109/ICCA.2013.6564958

@inproceedings{ee42028fd5854433a9cc67738d4a5245,

title = "Design of flight control system for a Hypersonic Gliding Vehicle based on nonlinear disturbance observer",

abstract = "Hypersonic Gliding Vehicle (HGV) is a new class of hypersonic glider being developed. This paper designs a flight control system for a Hypersonic Gliding Vehicle based on nonlinear disturbance observers. Firstly, a nonlinear disturbance observer (NDO) is used to estimate the unknown disturbances; the influence of disturbances is estimated by the NDO. Secondly, the NDO is integrated with a conventional sliding mode controller to compensate the influence of disturbances based on the estimate. Stability of the composite closed-loop system is provided using Lyapunov theory. Finally, simulation results present that the flight control system for the HGV achieves excellent results.",

author = "Chengshan Qian and Changyin Sun and Yiqing Huang and Chaoxu Mu and Jingmei Zhang and Ruimin Zhang",

year = "2013",

doi = "10.1109/ICCA.2013.6564958",

language = "英语",

isbn = "9781467347075",

series = "IEEE International Conference on Control and Automation, ICCA",

pages = "1573--1577",

booktitle = "2013 10th IEEE International Conference on Control and Automation, ICCA 2013",

note = "2013 10th IEEE International Conference on Control and Automation, ICCA 2013 ; Conference date: 12-06-2013 Through 14-06-2013",

}

Qian, C, Sun, C, Huang, Y, Mu, C, Zhang, J & Zhang, R 2013, Design of flight control system for a Hypersonic Gliding Vehicle based on nonlinear disturbance observer. in 2013 10th IEEE International Conference on Control and Automation, ICCA 2013., 6564958, IEEE International Conference on Control and Automation, ICCA, pp. 1573-1577, 2013 10th IEEE International Conference on Control and Automation, ICCA 2013, Hangzhou, China, 12/06/13. https://doi.org/10.1109/ICCA.2013.6564958

Design of flight control system for a Hypersonic Gliding Vehicle based on nonlinear disturbance observer. / Qian, Chengshan; Sun, Changyin; Huang, Yiqing et al.
2013 10th IEEE International Conference on Control and Automation, ICCA 2013. 2013. p. 1573-1577 6564958 (IEEE International Conference on Control and Automation, ICCA).

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

TY - GEN

T1 - Design of flight control system for a Hypersonic Gliding Vehicle based on nonlinear disturbance observer

AU - Qian, Chengshan

AU - Sun, Changyin

AU - Huang, Yiqing

AU - Mu, Chaoxu

AU - Zhang, Jingmei

AU - Zhang, Ruimin

PY - 2013

Y1 - 2013

N2 - Hypersonic Gliding Vehicle (HGV) is a new class of hypersonic glider being developed. This paper designs a flight control system for a Hypersonic Gliding Vehicle based on nonlinear disturbance observers. Firstly, a nonlinear disturbance observer (NDO) is used to estimate the unknown disturbances; the influence of disturbances is estimated by the NDO. Secondly, the NDO is integrated with a conventional sliding mode controller to compensate the influence of disturbances based on the estimate. Stability of the composite closed-loop system is provided using Lyapunov theory. Finally, simulation results present that the flight control system for the HGV achieves excellent results.

AB - Hypersonic Gliding Vehicle (HGV) is a new class of hypersonic glider being developed. This paper designs a flight control system for a Hypersonic Gliding Vehicle based on nonlinear disturbance observers. Firstly, a nonlinear disturbance observer (NDO) is used to estimate the unknown disturbances; the influence of disturbances is estimated by the NDO. Secondly, the NDO is integrated with a conventional sliding mode controller to compensate the influence of disturbances based on the estimate. Stability of the composite closed-loop system is provided using Lyapunov theory. Finally, simulation results present that the flight control system for the HGV achieves excellent results.

UR - https://www.scopus.com/pages/publications/84882303262

U2 - 10.1109/ICCA.2013.6564958

DO - 10.1109/ICCA.2013.6564958

M3 - 会议稿件

AN - SCOPUS:84882303262

SN - 9781467347075

T3 - IEEE International Conference on Control and Automation, ICCA

SP - 1573

EP - 1577

BT - 2013 10th IEEE International Conference on Control and Automation, ICCA 2013

T2 - 2013 10th IEEE International Conference on Control and Automation, ICCA 2013

Y2 - 12 June 2013 through 14 June 2013

ER -

Design of flight control system for a Hypersonic Gliding Vehicle based on nonlinear disturbance observer

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