Attitude synchronization of spacecraft formation flying via the SDRE controller using reaction wheels

Junoh Jung; Insu Chang; Sang Young Park

Attitude synchronization of spacecraft formation flying via the SDRE controller using reaction wheels

Junoh Jung, Insu Chang, Sang Young Park

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

Abstract

The objective of this study is to develop a decentralized control algorithm for attitude synchronization of spacecraft formation flying using Reaction Wheel Assembly (RWA). For the control, the absolute and relative dynamics with RWAs are formulated; these are used to construct the feedback controllers. The State-Dependent Riccati Equation (SDRE) technique is used to regulate state errors. In order to reduce the computational burden of solving the algebraic Riccati equation for relative motion, a parameter-dependent connectivity condition is suggested. The reliability of the proposed control law is validated by using a new system, which contains a Hardware-In-the-Loop Simulator (HILS). The experimental results show the effectiveness of the proposed control law.

Original language	English
Title of host publication	Spaceflight Mechanics 2010 - Advances in the Astronautical Sciences
Subtitle of host publication	Proceedings of the AAS/AIAA Space Flight Mechanics Meeting
Pages	2353-2369
Number of pages	17
Publication status	Published - 2010
Event	AAS/AIAA Space Flight Mechanics Meeting - San Diego, CA, United States Duration: 2010 Feb 14 → 2010 Feb 17

Publication series

Name	Advances in the Astronautical Sciences
Volume	136
ISSN (Print)	0065-3438

Other

Other	AAS/AIAA Space Flight Mechanics Meeting
Country/Territory	United States
City	San Diego, CA
Period	10/2/14 → 10/2/17

All Science Journal Classification (ASJC) codes

Aerospace Engineering
Space and Planetary Science

Cite this

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title = "Attitude synchronization of spacecraft formation flying via the SDRE controller using reaction wheels",

abstract = "The objective of this study is to develop a decentralized control algorithm for attitude synchronization of spacecraft formation flying using Reaction Wheel Assembly (RWA). For the control, the absolute and relative dynamics with RWAs are formulated; these are used to construct the feedback controllers. The State-Dependent Riccati Equation (SDRE) technique is used to regulate state errors. In order to reduce the computational burden of solving the algebraic Riccati equation for relative motion, a parameter-dependent connectivity condition is suggested. The reliability of the proposed control law is validated by using a new system, which contains a Hardware-In-the-Loop Simulator (HILS). The experimental results show the effectiveness of the proposed control law.",

author = "Junoh Jung and Insu Chang and Park, {Sang Young}",

year = "2010",

language = "English",

isbn = "9780877035602",

series = "Advances in the Astronautical Sciences",

pages = "2353--2369",

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note = "AAS/AIAA Space Flight Mechanics Meeting ; Conference date: 14-02-2010 Through 17-02-2010",

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Jung, J, Chang, I & Park, SY 2010, Attitude synchronization of spacecraft formation flying via the SDRE controller using reaction wheels. in Spaceflight Mechanics 2010 - Advances in the Astronautical Sciences: Proceedings of the AAS/AIAA Space Flight Mechanics Meeting. Advances in the Astronautical Sciences, vol. 136, pp. 2353-2369, AAS/AIAA Space Flight Mechanics Meeting, San Diego, CA, United States, 10/2/14.

Attitude synchronization of spacecraft formation flying via the SDRE controller using reaction wheels. / Jung, Junoh; Chang, Insu; Park, Sang Young.
Spaceflight Mechanics 2010 - Advances in the Astronautical Sciences: Proceedings of the AAS/AIAA Space Flight Mechanics Meeting. 2010. p. 2353-2369 (Advances in the Astronautical Sciences; Vol. 136).

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

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AB - The objective of this study is to develop a decentralized control algorithm for attitude synchronization of spacecraft formation flying using Reaction Wheel Assembly (RWA). For the control, the absolute and relative dynamics with RWAs are formulated; these are used to construct the feedback controllers. The State-Dependent Riccati Equation (SDRE) technique is used to regulate state errors. In order to reduce the computational burden of solving the algebraic Riccati equation for relative motion, a parameter-dependent connectivity condition is suggested. The reliability of the proposed control law is validated by using a new system, which contains a Hardware-In-the-Loop Simulator (HILS). The experimental results show the effectiveness of the proposed control law.

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Attitude synchronization of spacecraft formation flying via the SDRE controller using reaction wheels

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All Science Journal Classification (ASJC) codes

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