Singularity analysis and configuration optimization of two SGCMGs

Chengfei Yue; Cher Hiang Goh; Tong Heng Lee; Qiang Shen

doi:10.1109/AERO.2017.7943796

Singularity analysis and configuration optimization of two SGCMGs

Chengfei Yue
, Cher Hiang Goh
, Tong Heng Lee
, Qiang Shen

National University of Singapore

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

1 Scopus citations

Abstract

In contrast to past studies that treat each configuration of Single Gimbal Control Moment Gyros (SGCMGs) individually, this paper introduces a unified coordinate frame such that two SGCMGs in arbitrary configuration can be transformed into a unified description. Using this description, the angle between two fixed gimbal axes becomes the unique parameter to determine the shape of the momentum envelope and various singular surface, which offers the convenience for singularity analysis and configuration optimization. For different angles of two gimbal axes, we investigate its corresponding singularity and provide a thorough analysis. Consequently, this angle is optimized from the viewpoint of maximizing the momentum envelope. This work may lay foundation for the application of two SGCMGs in satellite attitude control.

Original language	English
Title of host publication	2017 IEEE Aerospace Conference
Publisher	IEEE Computer Society
ISBN (Electronic)	9781509016136
DOIs	https://doi.org/10.1109/AERO.2017.7943796
State	Published - 7 Jun 2017
Externally published	Yes
Event	2017 IEEE Aerospace Conference, AERO 2017 - Big Sky, United States Duration: 4 Mar 2017 → 11 Mar 2017

Publication series

Name	IEEE Aerospace Conference Proceedings
ISSN (Print)	1095-323X

Conference

Conference	2017 IEEE Aerospace Conference, AERO 2017
Country/Territory	United States
City	Big Sky
Period	4/03/17 → 11/03/17

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10.1109/AERO.2017.7943796

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@inproceedings{2d0666d5005a443fbec16d9a7218e35f,

title = "Singularity analysis and configuration optimization of two SGCMGs",

abstract = "In contrast to past studies that treat each configuration of Single Gimbal Control Moment Gyros (SGCMGs) individually, this paper introduces a unified coordinate frame such that two SGCMGs in arbitrary configuration can be transformed into a unified description. Using this description, the angle between two fixed gimbal axes becomes the unique parameter to determine the shape of the momentum envelope and various singular surface, which offers the convenience for singularity analysis and configuration optimization. For different angles of two gimbal axes, we investigate its corresponding singularity and provide a thorough analysis. Consequently, this angle is optimized from the viewpoint of maximizing the momentum envelope. This work may lay foundation for the application of two SGCMGs in satellite attitude control.",

author = "Chengfei Yue and Goh, \{Cher Hiang\} and Lee, \{Tong Heng\} and Qiang Shen",

note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 2017 IEEE Aerospace Conference, AERO 2017 ; Conference date: 04-03-2017 Through 11-03-2017",

year = "2017",

month = jun,

day = "7",

doi = "10.1109/AERO.2017.7943796",

language = "英语",

series = "IEEE Aerospace Conference Proceedings",

publisher = "IEEE Computer Society",

booktitle = "2017 IEEE Aerospace Conference",

address = "美国",

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TY - GEN

T1 - Singularity analysis and configuration optimization of two SGCMGs

AU - Yue, Chengfei

AU - Goh, Cher Hiang

AU - Lee, Tong Heng

AU - Shen, Qiang

PY - 2017/6/7

Y1 - 2017/6/7

N2 - In contrast to past studies that treat each configuration of Single Gimbal Control Moment Gyros (SGCMGs) individually, this paper introduces a unified coordinate frame such that two SGCMGs in arbitrary configuration can be transformed into a unified description. Using this description, the angle between two fixed gimbal axes becomes the unique parameter to determine the shape of the momentum envelope and various singular surface, which offers the convenience for singularity analysis and configuration optimization. For different angles of two gimbal axes, we investigate its corresponding singularity and provide a thorough analysis. Consequently, this angle is optimized from the viewpoint of maximizing the momentum envelope. This work may lay foundation for the application of two SGCMGs in satellite attitude control.

AB - In contrast to past studies that treat each configuration of Single Gimbal Control Moment Gyros (SGCMGs) individually, this paper introduces a unified coordinate frame such that two SGCMGs in arbitrary configuration can be transformed into a unified description. Using this description, the angle between two fixed gimbal axes becomes the unique parameter to determine the shape of the momentum envelope and various singular surface, which offers the convenience for singularity analysis and configuration optimization. For different angles of two gimbal axes, we investigate its corresponding singularity and provide a thorough analysis. Consequently, this angle is optimized from the viewpoint of maximizing the momentum envelope. This work may lay foundation for the application of two SGCMGs in satellite attitude control.

UR - https://www.scopus.com/pages/publications/85021239249

U2 - 10.1109/AERO.2017.7943796

DO - 10.1109/AERO.2017.7943796

M3 - 会议稿件

AN - SCOPUS:85021239249

T3 - IEEE Aerospace Conference Proceedings

BT - 2017 IEEE Aerospace Conference

PB - IEEE Computer Society

T2 - 2017 IEEE Aerospace Conference, AERO 2017

Y2 - 4 March 2017 through 11 March 2017

ER -

Singularity analysis and configuration optimization of two SGCMGs

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