Disturbance observer based constrained multi-model predictive control for Mars entry trajectory tracking

Chao Wu; Shihua Li; Jun Yang; Lei Guo

doi:10.1109/CGNCC.2014.7007534

Disturbance observer based constrained multi-model predictive control for Mars entry trajectory tracking

Chao Wu
, Shihua Li
, Jun Yang
, Lei Guo

自动化科学与电气工程学院

Southeast University, Nanjing

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

2 引用（Scopus）

摘要

For future Mars entry missions, a composite entry tracking strategy is studied in this article. For precision entry, the nonlinear entry dynamics, complex uncertainties and multi-source disturbance are considered specially. The composite entry tracking strategy includes constrained multi-model predictive control (CMPC), to optimize tracking performance, as well as disturbance observer based control for active disturbance rejection. Monte Carlo simulations demonstrate the effectiveness of the proposed method under control saturation constraint, multi-source disturbances and uncertainties of initial states and aerodynamic parameters.

源语言	英语
主期刊名	2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
出版商	Institute of Electrical and Electronics Engineers Inc.
页	2341-2346
页数	6
ISBN（电子版）	9781479946990
DOI	https://doi.org/10.1109/CGNCC.2014.7007534
出版状态	已出版 - 12 1月 2015
活动	6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 - Yantai, 中国期限: 8 8月 2014 → 10 8月 2014

出版系列

姓名	2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

会议

会议	6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
国家/地区	中国
市	Yantai
时期	8/08/14 → 10/08/14

访问文件

10.1109/CGNCC.2014.7007534

其它文件与链接

链接到 Scopus 的出版物

引用此

Wu, C., Li, S., Yang, J., & Guo, L. (2015). Disturbance observer based constrained multi-model predictive control for Mars entry trajectory tracking. 在 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 (页码 2341-2346). 文章 7007534 (2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CGNCC.2014.7007534

Wu, Chao ; Li, Shihua ; Yang, Jun 等. / Disturbance observer based constrained multi-model predictive control for Mars entry trajectory tracking. 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014. Institute of Electrical and Electronics Engineers Inc., 2015. 页码 2341-2346 (2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014).

@inproceedings{bd83c9c806a8484db7d1ba1f58354feb,

title = "Disturbance observer based constrained multi-model predictive control for Mars entry trajectory tracking",

abstract = "For future Mars entry missions, a composite entry tracking strategy is studied in this article. For precision entry, the nonlinear entry dynamics, complex uncertainties and multi-source disturbance are considered specially. The composite entry tracking strategy includes constrained multi-model predictive control (CMPC), to optimize tracking performance, as well as disturbance observer based control for active disturbance rejection. Monte Carlo simulations demonstrate the effectiveness of the proposed method under control saturation constraint, multi-source disturbances and uncertainties of initial states and aerodynamic parameters.",

author = "Chao Wu and Shihua Li and Jun Yang and Lei Guo",

note = "Publisher Copyright: {\textcopyright} 2014 IEEE.; 6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 ; Conference date: 08-08-2014 Through 10-08-2014",

year = "2015",

month = jan,

day = "12",

doi = "10.1109/CGNCC.2014.7007534",

language = "英语",

series = "2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014",

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

pages = "2341--2346",

booktitle = "2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014",

address = "美国",

}

Wu, C, Li, S, Yang, J & Guo, L 2015, Disturbance observer based constrained multi-model predictive control for Mars entry trajectory tracking. 在 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014., 7007534, 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014, Institute of Electrical and Electronics Engineers Inc., 页码 2341-2346, 6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014, Yantai, 中国, 8/08/14. https://doi.org/10.1109/CGNCC.2014.7007534

Disturbance observer based constrained multi-model predictive control for Mars entry trajectory tracking. / Wu, Chao; Li, Shihua; Yang, Jun 等.
2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014. Institute of Electrical and Electronics Engineers Inc., 2015. 页码 2341-2346 7007534 (2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014).

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

TY - GEN

T1 - Disturbance observer based constrained multi-model predictive control for Mars entry trajectory tracking

AU - Wu, Chao

AU - Li, Shihua

AU - Yang, Jun

AU - Guo, Lei

PY - 2015/1/12

Y1 - 2015/1/12

N2 - For future Mars entry missions, a composite entry tracking strategy is studied in this article. For precision entry, the nonlinear entry dynamics, complex uncertainties and multi-source disturbance are considered specially. The composite entry tracking strategy includes constrained multi-model predictive control (CMPC), to optimize tracking performance, as well as disturbance observer based control for active disturbance rejection. Monte Carlo simulations demonstrate the effectiveness of the proposed method under control saturation constraint, multi-source disturbances and uncertainties of initial states and aerodynamic parameters.

AB - For future Mars entry missions, a composite entry tracking strategy is studied in this article. For precision entry, the nonlinear entry dynamics, complex uncertainties and multi-source disturbance are considered specially. The composite entry tracking strategy includes constrained multi-model predictive control (CMPC), to optimize tracking performance, as well as disturbance observer based control for active disturbance rejection. Monte Carlo simulations demonstrate the effectiveness of the proposed method under control saturation constraint, multi-source disturbances and uncertainties of initial states and aerodynamic parameters.

UR - https://www.scopus.com/pages/publications/84922581948

U2 - 10.1109/CGNCC.2014.7007534

DO - 10.1109/CGNCC.2014.7007534

M3 - 会议稿件

AN - SCOPUS:84922581948

T3 - 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

SP - 2341

EP - 2346

BT - 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

Y2 - 8 August 2014 through 10 August 2014

ER -

Wu C, Li S, Yang J, Guo L. Disturbance observer based constrained multi-model predictive control for Mars entry trajectory tracking. 在 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014. Institute of Electrical and Electronics Engineers Inc. 2015. 页码 2341-2346. 7007534. (2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014). doi: 10.1109/CGNCC.2014.7007534

Disturbance observer based constrained multi-model predictive control for Mars entry trajectory tracking

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