Observability analysis of autonomous navigation system of interplanetary spacecraft

Xiaohua Chang; Pingyuan Cui; Hutao Cui

doi:10.1109/CCDC.2009.5191866

Observability analysis of autonomous navigation system of interplanetary spacecraft

Xiaohua Chang^*
, Pingyuan Cui
, Hutao Cui

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

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

2 Scopus citations

Abstract

In this paper, an autonomous navigation scheme for interplanetary spacecraft based on the Sun line-of-sight vector measurement is proposed. In order to prove that the directional data alone can completely determine the spacecraft orbit, an analytical observability analysis is implemented through the partial derivative of the measurement equation. Then, a numerical local observability analysis is derived from the Lie derivative. Also presented is a global observability analysis by introducing the condition number of the measurement matrix. Finally, simulation results demonstrate the validity of the proposed navigation algorithm.

Original language	English
Title of host publication	2009 Chinese Control and Decision Conference, CCDC 2009
Pages	766-770
Number of pages	5
DOIs	https://doi.org/10.1109/CCDC.2009.5191866
State	Published - 2009
Event	2009 Chinese Control and Decision Conference, CCDC 2009 - Guilin, China Duration: 17 Jun 2009 → 19 Jun 2009

Publication series

Name	2009 Chinese Control and Decision Conference, CCDC 2009

Conference

Conference	2009 Chinese Control and Decision Conference, CCDC 2009
Country/Territory	China
City	Guilin
Period	17/06/09 → 19/06/09

Keywords

Autonomous navigation
Condition number
Observability

Access to Document

10.1109/CCDC.2009.5191866

Cite this

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title = "Observability analysis of autonomous navigation system of interplanetary spacecraft",

abstract = "In this paper, an autonomous navigation scheme for interplanetary spacecraft based on the Sun line-of-sight vector measurement is proposed. In order to prove that the directional data alone can completely determine the spacecraft orbit, an analytical observability analysis is implemented through the partial derivative of the measurement equation. Then, a numerical local observability analysis is derived from the Lie derivative. Also presented is a global observability analysis by introducing the condition number of the measurement matrix. Finally, simulation results demonstrate the validity of the proposed navigation algorithm.",

keywords = "Autonomous navigation, Condition number, Observability",

author = "Xiaohua Chang and Pingyuan Cui and Hutao Cui",

year = "2009",

doi = "10.1109/CCDC.2009.5191866",

language = "英语",

isbn = "9781424427239",

series = "2009 Chinese Control and Decision Conference, CCDC 2009",

pages = "766--770",

booktitle = "2009 Chinese Control and Decision Conference, CCDC 2009",

note = "2009 Chinese Control and Decision Conference, CCDC 2009 ; Conference date: 17-06-2009 Through 19-06-2009",

}

Chang, X, Cui, P & Cui, H 2009, Observability analysis of autonomous navigation system of interplanetary spacecraft. in 2009 Chinese Control and Decision Conference, CCDC 2009., 5191866, 2009 Chinese Control and Decision Conference, CCDC 2009, pp. 766-770, 2009 Chinese Control and Decision Conference, CCDC 2009, Guilin, China, 17/06/09. https://doi.org/10.1109/CCDC.2009.5191866

Observability analysis of autonomous navigation system of interplanetary spacecraft. / Chang, Xiaohua; Cui, Pingyuan; Cui, Hutao.
2009 Chinese Control and Decision Conference, CCDC 2009. 2009. p. 766-770 5191866 (2009 Chinese Control and Decision Conference, CCDC 2009).

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

TY - GEN

T1 - Observability analysis of autonomous navigation system of interplanetary spacecraft

AU - Chang, Xiaohua

AU - Cui, Pingyuan

AU - Cui, Hutao

PY - 2009

Y1 - 2009

N2 - In this paper, an autonomous navigation scheme for interplanetary spacecraft based on the Sun line-of-sight vector measurement is proposed. In order to prove that the directional data alone can completely determine the spacecraft orbit, an analytical observability analysis is implemented through the partial derivative of the measurement equation. Then, a numerical local observability analysis is derived from the Lie derivative. Also presented is a global observability analysis by introducing the condition number of the measurement matrix. Finally, simulation results demonstrate the validity of the proposed navigation algorithm.

AB - In this paper, an autonomous navigation scheme for interplanetary spacecraft based on the Sun line-of-sight vector measurement is proposed. In order to prove that the directional data alone can completely determine the spacecraft orbit, an analytical observability analysis is implemented through the partial derivative of the measurement equation. Then, a numerical local observability analysis is derived from the Lie derivative. Also presented is a global observability analysis by introducing the condition number of the measurement matrix. Finally, simulation results demonstrate the validity of the proposed navigation algorithm.

KW - Autonomous navigation

KW - Condition number

KW - Observability

UR - https://www.scopus.com/pages/publications/70449473546

U2 - 10.1109/CCDC.2009.5191866

DO - 10.1109/CCDC.2009.5191866

M3 - 会议稿件

AN - SCOPUS:70449473546

SN - 9781424427239

T3 - 2009 Chinese Control and Decision Conference, CCDC 2009

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EP - 770

BT - 2009 Chinese Control and Decision Conference, CCDC 2009

T2 - 2009 Chinese Control and Decision Conference, CCDC 2009

Y2 - 17 June 2009 through 19 June 2009

ER -

Observability analysis of autonomous navigation system of interplanetary spacecraft

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