A study on biased guidance problem of the space flight vehicle

Xi Zhang; Yu Yao; Fenghua He

doi:10.1109/ChiCC.2016.7554241

A study on biased guidance problem of the space flight vehicle

Xi Zhang
, Yu Yao
, Fenghua He

School of Astronautics

Harbin Institute of Technology

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

4 Scopus citations

Abstract

In this manuscript, in order to realize a close-up observation for a space target, the biased guidance problem is investigated, which aims to achieve a controlled nonzero minimum relative distance between the space flight vehicle and the target, named as the biased distance. First, the relative motion model is established and the biased guidance control index is proposed, based on which the missing-target-point, where the flight vehicle loses the sight of the target, is given and the phase division of the biased guidance process is determined. Secondly, the biased guidance law based on proportional navigation method is proposed and the Lyapunov stability is proved. Thirdly, the errors of the biased distance caused by the control index and the erroneous detection information are given respectively. Finally, some simulations are carried out to illustrate the effectiveness of the proposed biased guidance law and the errors of the biased distance under different conditions are given.

Original language	English
Title of host publication	Proceedings of the 35th Chinese Control Conference, CCC 2016
Editors	Jie Chen, Qianchuan Zhao, Jie Chen
Publisher	IEEE Computer Society
Pages	5671-5676
Number of pages	6
ISBN (Electronic)	9789881563910
DOIs	https://doi.org/10.1109/ChiCC.2016.7554241
State	Published - 26 Aug 2016
Event	35th Chinese Control Conference, CCC 2016 - Chengdu, China Duration: 27 Jul 2016 → 29 Jul 2016

Publication series

Name	Chinese Control Conference, CCC
Volume	2016-August
ISSN (Print)	1934-1768
ISSN (Electronic)	2161-2927

Conference

Conference	35th Chinese Control Conference, CCC 2016
Country/Territory	China
City	Chengdu
Period	27/07/16 → 29/07/16

Keywords

Biased Guidance
Close-up Observation
Guidance Error
Guidance Law Design

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10.1109/ChiCC.2016.7554241

Cite this

@inproceedings{3374510ded6347a58dfa8f51512eb28c,

title = "A study on biased guidance problem of the space flight vehicle",

abstract = "In this manuscript, in order to realize a close-up observation for a space target, the biased guidance problem is investigated, which aims to achieve a controlled nonzero minimum relative distance between the space flight vehicle and the target, named as the biased distance. First, the relative motion model is established and the biased guidance control index is proposed, based on which the missing-target-point, where the flight vehicle loses the sight of the target, is given and the phase division of the biased guidance process is determined. Secondly, the biased guidance law based on proportional navigation method is proposed and the Lyapunov stability is proved. Thirdly, the errors of the biased distance caused by the control index and the erroneous detection information are given respectively. Finally, some simulations are carried out to illustrate the effectiveness of the proposed biased guidance law and the errors of the biased distance under different conditions are given.",

keywords = "Biased Guidance, Close-up Observation, Guidance Error, Guidance Law Design",

author = "Xi Zhang and Yu Yao and Fenghua He",

note = "Publisher Copyright: {\textcopyright} 2016 TCCT.; 35th Chinese Control Conference, CCC 2016 ; Conference date: 27-07-2016 Through 29-07-2016",

year = "2016",

month = aug,

day = "26",

doi = "10.1109/ChiCC.2016.7554241",

language = "英语",

series = "Chinese Control Conference, CCC",

publisher = "IEEE Computer Society",

pages = "5671--5676",

editor = "Jie Chen and Qianchuan Zhao and Jie Chen",

booktitle = "Proceedings of the 35th Chinese Control Conference, CCC 2016",

address = "美国",

}

Zhang, X, Yao, Y & He, F 2016, A study on biased guidance problem of the space flight vehicle. in J Chen, Q Zhao & J Chen (eds), Proceedings of the 35th Chinese Control Conference, CCC 2016., 7554241, Chinese Control Conference, CCC, vol. 2016-August, IEEE Computer Society, pp. 5671-5676, 35th Chinese Control Conference, CCC 2016, Chengdu, China, 27/07/16. https://doi.org/10.1109/ChiCC.2016.7554241

A study on biased guidance problem of the space flight vehicle. / Zhang, Xi; Yao, Yu; He, Fenghua.
Proceedings of the 35th Chinese Control Conference, CCC 2016. ed. / Jie Chen; Qianchuan Zhao; Jie Chen. IEEE Computer Society, 2016. p. 5671-5676 7554241 (Chinese Control Conference, CCC; Vol. 2016-August).

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

TY - GEN

T1 - A study on biased guidance problem of the space flight vehicle

AU - Zhang, Xi

AU - Yao, Yu

AU - He, Fenghua

PY - 2016/8/26

Y1 - 2016/8/26

N2 - In this manuscript, in order to realize a close-up observation for a space target, the biased guidance problem is investigated, which aims to achieve a controlled nonzero minimum relative distance between the space flight vehicle and the target, named as the biased distance. First, the relative motion model is established and the biased guidance control index is proposed, based on which the missing-target-point, where the flight vehicle loses the sight of the target, is given and the phase division of the biased guidance process is determined. Secondly, the biased guidance law based on proportional navigation method is proposed and the Lyapunov stability is proved. Thirdly, the errors of the biased distance caused by the control index and the erroneous detection information are given respectively. Finally, some simulations are carried out to illustrate the effectiveness of the proposed biased guidance law and the errors of the biased distance under different conditions are given.

AB - In this manuscript, in order to realize a close-up observation for a space target, the biased guidance problem is investigated, which aims to achieve a controlled nonzero minimum relative distance between the space flight vehicle and the target, named as the biased distance. First, the relative motion model is established and the biased guidance control index is proposed, based on which the missing-target-point, where the flight vehicle loses the sight of the target, is given and the phase division of the biased guidance process is determined. Secondly, the biased guidance law based on proportional navigation method is proposed and the Lyapunov stability is proved. Thirdly, the errors of the biased distance caused by the control index and the erroneous detection information are given respectively. Finally, some simulations are carried out to illustrate the effectiveness of the proposed biased guidance law and the errors of the biased distance under different conditions are given.

KW - Biased Guidance

KW - Close-up Observation

KW - Guidance Error

KW - Guidance Law Design

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M3 - 会议稿件

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BT - Proceedings of the 35th Chinese Control Conference, CCC 2016

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PB - IEEE Computer Society

T2 - 35th Chinese Control Conference, CCC 2016

Y2 - 27 July 2016 through 29 July 2016

ER -

A study on biased guidance problem of the space flight vehicle

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