Entry trajectory optimization for hypersonic vehicle based on time-scales separation guidance with waterweeds algorithm

Xudong Liu; Lin Cheng; Qingzhen Zhang; Lingtong Jiang

doi:10.1109/CGNCC.2016.7828785

Entry trajectory optimization for hypersonic vehicle based on time-scales separation guidance with waterweeds algorithm

Xudong Liu^*
, Lin Cheng
, Qingzhen Zhang
, Lingtong Jiang

^*Corresponding author for this work

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

5 Scopus citations

Abstract

This paper focuses on the hypersonic vehicle in consideration of oscillation and aerodynamic heating problems during reentry process, for trajectory optimization, penalty function method and ϵ level comparison are introduced for transforming the unconstrained waterweeds algorithm into constrained algorithm to solve multi-objective optimization problems, in which a novel and more precise criterion based on time-scales separation guidance for oscillation optimization is put forward indicating waterweeds algorithm to get a better optimal result. The algorithm transformed is successfully applied to trajectory design.

Original language	English
Title of host publication	CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	209-215
Number of pages	7
ISBN (Electronic)	9781467383189
DOIs	https://doi.org/10.1109/CGNCC.2016.7828785
State	Published - 20 Jan 2017
Event	7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016 - Nanjing, Jiangsu, China Duration: 12 Aug 2016 → 14 Aug 2016

Publication series

Name	CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference

Conference

Conference	7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016
Country/Territory	China
City	Nanjing, Jiangsu
Period	12/08/16 → 14/08/16

Access to Document

10.1109/CGNCC.2016.7828785

Cite this

Liu, X., Cheng, L., Zhang, Q., & Jiang, L. (2017). Entry trajectory optimization for hypersonic vehicle based on time-scales separation guidance with waterweeds algorithm. In CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference (pp. 209-215). Article 7828785 (CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CGNCC.2016.7828785

Liu, Xudong ; Cheng, Lin ; Zhang, Qingzhen et al. / Entry trajectory optimization for hypersonic vehicle based on time-scales separation guidance with waterweeds algorithm. CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference. Institute of Electrical and Electronics Engineers Inc., 2017. pp. 209-215 (CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference).

@inproceedings{7fb0d704428945a9b0b7a963db8ebfd6,

title = "Entry trajectory optimization for hypersonic vehicle based on time-scales separation guidance with waterweeds algorithm",

abstract = "This paper focuses on the hypersonic vehicle in consideration of oscillation and aerodynamic heating problems during reentry process, for trajectory optimization, penalty function method and ϵ level comparison are introduced for transforming the unconstrained waterweeds algorithm into constrained algorithm to solve multi-objective optimization problems, in which a novel and more precise criterion based on time-scales separation guidance for oscillation optimization is put forward indicating waterweeds algorithm to get a better optimal result. The algorithm transformed is successfully applied to trajectory design.",

author = "Xudong Liu and Lin Cheng and Qingzhen Zhang and Lingtong Jiang",

note = "Publisher Copyright: {\textcopyright} 2016 IEEE.; 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016 ; Conference date: 12-08-2016 Through 14-08-2016",

year = "2017",

month = jan,

day = "20",

doi = "10.1109/CGNCC.2016.7828785",

language = "英语",

series = "CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference",

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

pages = "209--215",

booktitle = "CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference",

address = "美国",

}

Liu, X , Cheng, L , Zhang, Q & Jiang, L 2017, Entry trajectory optimization for hypersonic vehicle based on time-scales separation guidance with waterweeds algorithm. in CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference., 7828785, CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference, Institute of Electrical and Electronics Engineers Inc., pp. 209-215, 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016, Nanjing, Jiangsu, China, 12/08/16. https://doi.org/10.1109/CGNCC.2016.7828785

Entry trajectory optimization for hypersonic vehicle based on time-scales separation guidance with waterweeds algorithm. / Liu, Xudong ; Cheng, Lin ; Zhang, Qingzhen et al.
CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference. Institute of Electrical and Electronics Engineers Inc., 2017. p. 209-215 7828785 (CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference).

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

TY - GEN

T1 - Entry trajectory optimization for hypersonic vehicle based on time-scales separation guidance with waterweeds algorithm

AU - Liu, Xudong

AU - Cheng, Lin

AU - Zhang, Qingzhen

AU - Jiang, Lingtong

PY - 2017/1/20

Y1 - 2017/1/20

N2 - This paper focuses on the hypersonic vehicle in consideration of oscillation and aerodynamic heating problems during reentry process, for trajectory optimization, penalty function method and ϵ level comparison are introduced for transforming the unconstrained waterweeds algorithm into constrained algorithm to solve multi-objective optimization problems, in which a novel and more precise criterion based on time-scales separation guidance for oscillation optimization is put forward indicating waterweeds algorithm to get a better optimal result. The algorithm transformed is successfully applied to trajectory design.

AB - This paper focuses on the hypersonic vehicle in consideration of oscillation and aerodynamic heating problems during reentry process, for trajectory optimization, penalty function method and ϵ level comparison are introduced for transforming the unconstrained waterweeds algorithm into constrained algorithm to solve multi-objective optimization problems, in which a novel and more precise criterion based on time-scales separation guidance for oscillation optimization is put forward indicating waterweeds algorithm to get a better optimal result. The algorithm transformed is successfully applied to trajectory design.

UR - https://www.scopus.com/pages/publications/85015231665

U2 - 10.1109/CGNCC.2016.7828785

DO - 10.1109/CGNCC.2016.7828785

M3 - 会议稿件

AN - SCOPUS:85015231665

T3 - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference

SP - 209

EP - 215

BT - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016

Y2 - 12 August 2016 through 14 August 2016

ER -

Liu X , Cheng L , Zhang Q, Jiang L. Entry trajectory optimization for hypersonic vehicle based on time-scales separation guidance with waterweeds algorithm. In CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference. Institute of Electrical and Electronics Engineers Inc. 2017. p. 209-215. 7828785. (CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference). doi: 10.1109/CGNCC.2016.7828785

Entry trajectory optimization for hypersonic vehicle based on time-scales separation guidance with waterweeds algorithm

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