Research on Integrated Design of Guidance and Control for Hypersonic Vehicle Based on Trajectory Linearization Control Method

Yao De-Qing; Wei Yi-Yin; Cui Nai-Gang

doi:10.1109/ICUS48101.2019.8996033

Research on Integrated Design of Guidance and Control for Hypersonic Vehicle Based on Trajectory Linearization Control Method

Yao De-Qing
, Wei Yi-Yin
, Cui Nai-Gang

School of Astronautics, Harbin Institute of Technology

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

4 Scopus citations

Abstract

With the development of hypersonic technology, more attention should be paid on the research of integrated design of hypersonic guidance and control system. In this paper, the integrated lift-body hypersonic vehicle is taken as the research object, considering the unique flight dynamic characteristics which include fast time-varying, highly coupled, nonlinear, and uncertain characteristics, an integrated guidance and control design method based on the trajectory linearization control method is designed. The simulation results show that the method is effective and reliable, which can ensure the tracking performance and anti-disturbance ability in complex flight environment.

Original language	English
Title of host publication	Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	450-456
Number of pages	7
ISBN (Electronic)	9781728137926
DOIs	https://doi.org/10.1109/ICUS48101.2019.8996033
State	Published - Oct 2019
Externally published	Yes
Event	2019 IEEE International Conference on Unmanned Systems, ICUS 2019 - Beijing, China Duration: 17 Oct 2019 → 19 Oct 2019

Publication series

Name	Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019

Conference

Conference	2019 IEEE International Conference on Unmanned Systems, ICUS 2019
Country/Territory	China
City	Beijing
Period	17/10/19 → 19/10/19

Keywords

hypersonic vehicle
integrated guidance and control design method
simulation
trajectory linearization control

Access to Document

10.1109/ICUS48101.2019.8996033

Cite this

De-Qing, Y., Yi-Yin, W., & Nai-Gang, C. (2019). Research on Integrated Design of Guidance and Control for Hypersonic Vehicle Based on Trajectory Linearization Control Method. In Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019 (pp. 450-456). Article 8996033 (Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICUS48101.2019.8996033

De-Qing, Yao ; Yi-Yin, Wei ; Nai-Gang, Cui. / Research on Integrated Design of Guidance and Control for Hypersonic Vehicle Based on Trajectory Linearization Control Method. Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019. Institute of Electrical and Electronics Engineers Inc., 2019. pp. 450-456 (Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019).

@inproceedings{42b49f8a19d543809a3fed6758619899,

title = "Research on Integrated Design of Guidance and Control for Hypersonic Vehicle Based on Trajectory Linearization Control Method",

abstract = "With the development of hypersonic technology, more attention should be paid on the research of integrated design of hypersonic guidance and control system. In this paper, the integrated lift-body hypersonic vehicle is taken as the research object, considering the unique flight dynamic characteristics which include fast time-varying, highly coupled, nonlinear, and uncertain characteristics, an integrated guidance and control design method based on the trajectory linearization control method is designed. The simulation results show that the method is effective and reliable, which can ensure the tracking performance and anti-disturbance ability in complex flight environment.",

keywords = "hypersonic vehicle, integrated guidance and control design method, simulation, trajectory linearization control",

author = "Yao De-Qing and Wei Yi-Yin and Cui Nai-Gang",

note = "Publisher Copyright: {\textcopyright} 2019 IEEE.; 2019 IEEE International Conference on Unmanned Systems, ICUS 2019 ; Conference date: 17-10-2019 Through 19-10-2019",

year = "2019",

month = oct,

doi = "10.1109/ICUS48101.2019.8996033",

language = "英语",

series = "Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

pages = "450--456",

booktitle = "Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019",

address = "美国",

}

De-Qing, Y, Yi-Yin, W & Nai-Gang, C 2019, Research on Integrated Design of Guidance and Control for Hypersonic Vehicle Based on Trajectory Linearization Control Method. in Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019., 8996033, Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019, Institute of Electrical and Electronics Engineers Inc., pp. 450-456, 2019 IEEE International Conference on Unmanned Systems, ICUS 2019, Beijing, China, 17/10/19. https://doi.org/10.1109/ICUS48101.2019.8996033

Research on Integrated Design of Guidance and Control for Hypersonic Vehicle Based on Trajectory Linearization Control Method. / De-Qing, Yao; Yi-Yin, Wei; Nai-Gang, Cui.
Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019. Institute of Electrical and Electronics Engineers Inc., 2019. p. 450-456 8996033 (Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019).

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

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AB - With the development of hypersonic technology, more attention should be paid on the research of integrated design of hypersonic guidance and control system. In this paper, the integrated lift-body hypersonic vehicle is taken as the research object, considering the unique flight dynamic characteristics which include fast time-varying, highly coupled, nonlinear, and uncertain characteristics, an integrated guidance and control design method based on the trajectory linearization control method is designed. The simulation results show that the method is effective and reliable, which can ensure the tracking performance and anti-disturbance ability in complex flight environment.

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KW - trajectory linearization control

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De-Qing Y, Yi-Yin W, Nai-Gang C. Research on Integrated Design of Guidance and Control for Hypersonic Vehicle Based on Trajectory Linearization Control Method. In Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019. Institute of Electrical and Electronics Engineers Inc. 2019. p. 450-456. 8996033. (Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019). doi: 10.1109/ICUS48101.2019.8996033

Research on Integrated Design of Guidance and Control for Hypersonic Vehicle Based on Trajectory Linearization Control Method

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