Simulations of spacecraft attitude control for tracking maneuvers with MATLAB and STK

Xiang Fang; Yunhai Geng

doi:10.1109/ICInfA.2014.6932824

Simulations of spacecraft attitude control for tracking maneuvers with MATLAB and STK

Xiang Fang
, Yunhai Geng

School of Astronautics

Harbin Institute of Technology

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

6 Scopus citations

Abstract

The spacecraft attitude tracking control problem and its MATLAB-STK simulation is researched in this paper. First, an attitude dynamic modal for tracking maneuvers based on error quaternion is established. And based on this dynamic modal a sliding mode variable structure controller is designed. Then, a simulation and visualization based on MATLAB-STK is finished. By ordering MATLAB to call for STK/Connect module, data can be communicate in both software. And it makes visualization of simulation result very easily in STK. The Simulation illustrate the performance of the proposed controllers.

Original language	English
Title of host publication	2014 IEEE International Conference on Information and Automation, ICIA 2014
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	1160-1165
Number of pages	6
ISBN (Electronic)	9781479941001
DOIs	https://doi.org/10.1109/ICInfA.2014.6932824
State	Published - 21 Oct 2014
Event	2014 IEEE International Conference on Information and Automation, ICIA 2014 - Hailar, Hulunbuir, China Duration: 28 Jul 2014 → 30 Jul 2014

Publication series

Name	2014 IEEE International Conference on Information and Automation, ICIA 2014

Conference

Conference	2014 IEEE International Conference on Information and Automation, ICIA 2014
Country/Territory	China
City	Hailar, Hulunbuir
Period	28/07/14 → 30/07/14

Keywords

Attitude Control for Tracking Maneuvers
MATLAB-STK Simulation and Visualization
Sliding Mode Variable Structure Control

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10.1109/ICInfA.2014.6932824

Cite this

Fang, X., & Geng, Y. (2014). Simulations of spacecraft attitude control for tracking maneuvers with MATLAB and STK. In 2014 IEEE International Conference on Information and Automation, ICIA 2014 (pp. 1160-1165). Article 6932824 (2014 IEEE International Conference on Information and Automation, ICIA 2014). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICInfA.2014.6932824

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title = "Simulations of spacecraft attitude control for tracking maneuvers with MATLAB and STK",

abstract = "The spacecraft attitude tracking control problem and its MATLAB-STK simulation is researched in this paper. First, an attitude dynamic modal for tracking maneuvers based on error quaternion is established. And based on this dynamic modal a sliding mode variable structure controller is designed. Then, a simulation and visualization based on MATLAB-STK is finished. By ordering MATLAB to call for STK/Connect module, data can be communicate in both software. And it makes visualization of simulation result very easily in STK. The Simulation illustrate the performance of the proposed controllers.",

keywords = "Attitude Control for Tracking Maneuvers, MATLAB-STK Simulation and Visualization, Sliding Mode Variable Structure Control",

author = "Xiang Fang and Yunhai Geng",

note = "Publisher Copyright: {\textcopyright} 2014 IEEE.; 2014 IEEE International Conference on Information and Automation, ICIA 2014 ; Conference date: 28-07-2014 Through 30-07-2014",

year = "2014",

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doi = "10.1109/ICInfA.2014.6932824",

language = "英语",

series = "2014 IEEE International Conference on Information and Automation, ICIA 2014",

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Fang, X & Geng, Y 2014, Simulations of spacecraft attitude control for tracking maneuvers with MATLAB and STK. in 2014 IEEE International Conference on Information and Automation, ICIA 2014., 6932824, 2014 IEEE International Conference on Information and Automation, ICIA 2014, Institute of Electrical and Electronics Engineers Inc., pp. 1160-1165, 2014 IEEE International Conference on Information and Automation, ICIA 2014, Hailar, Hulunbuir, China, 28/07/14. https://doi.org/10.1109/ICInfA.2014.6932824

Simulations of spacecraft attitude control for tracking maneuvers with MATLAB and STK. / Fang, Xiang; Geng, Yunhai.
2014 IEEE International Conference on Information and Automation, ICIA 2014. Institute of Electrical and Electronics Engineers Inc., 2014. p. 1160-1165 6932824 (2014 IEEE International Conference on Information and Automation, ICIA 2014).

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

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AU - Geng, Yunhai

PY - 2014/10/21

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N2 - The spacecraft attitude tracking control problem and its MATLAB-STK simulation is researched in this paper. First, an attitude dynamic modal for tracking maneuvers based on error quaternion is established. And based on this dynamic modal a sliding mode variable structure controller is designed. Then, a simulation and visualization based on MATLAB-STK is finished. By ordering MATLAB to call for STK/Connect module, data can be communicate in both software. And it makes visualization of simulation result very easily in STK. The Simulation illustrate the performance of the proposed controllers.

AB - The spacecraft attitude tracking control problem and its MATLAB-STK simulation is researched in this paper. First, an attitude dynamic modal for tracking maneuvers based on error quaternion is established. And based on this dynamic modal a sliding mode variable structure controller is designed. Then, a simulation and visualization based on MATLAB-STK is finished. By ordering MATLAB to call for STK/Connect module, data can be communicate in both software. And it makes visualization of simulation result very easily in STK. The Simulation illustrate the performance of the proposed controllers.

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KW - MATLAB-STK Simulation and Visualization

KW - Sliding Mode Variable Structure Control

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BT - 2014 IEEE International Conference on Information and Automation, ICIA 2014

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2014 IEEE International Conference on Information and Automation, ICIA 2014

Y2 - 28 July 2014 through 30 July 2014

ER -

Fang X, Geng Y. Simulations of spacecraft attitude control for tracking maneuvers with MATLAB and STK. In 2014 IEEE International Conference on Information and Automation, ICIA 2014. Institute of Electrical and Electronics Engineers Inc. 2014. p. 1160-1165. 6932824. (2014 IEEE International Conference on Information and Automation, ICIA 2014). doi: 10.1109/ICInfA.2014.6932824

Simulations of spacecraft attitude control for tracking maneuvers with MATLAB and STK

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