Guidance and control for satellite in-orbit-self-assembly proximity operations

Guidance and control for satellite in-orbit-self-assembly proximity operations

In this paper, the autonomous in-orbit-self-assembly of multiple satellites is exploited in close proximity operations. Guidance and control algorithms are developed based on the closed-form analytical solution of relative motion equations that is completely explicit in time in a general Keplerian o...

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Main Authors: Okasha, Mohamed Elsayed Aly Abd Elaziz, Park, Chandeok, Park, Sang-Young
Format: Article
Language:English
Published: Elsevier Masson SAS 2015
Subjects:
TL500 Aeronautics
TL787 Astronautics
Online Access:http://irep.iium.edu.my/41283/
http://irep.iium.edu.my/41283/
http://irep.iium.edu.my/41283/
http://irep.iium.edu.my/41283/1/1-s2.0-S1270963814002569-main.pdf
id iium-41283
recordtype eprints
spelling iium-412832016-05-16T02:19:22Z http://irep.iium.edu.my/41283/ Guidance and control for satellite in-orbit-self-assembly proximity operations Okasha, Mohamed Elsayed Aly Abd Elaziz Park, Chandeok Park, Sang-Young TL500 Aeronautics TL787 Astronautics In this paper, the autonomous in-orbit-self-assembly of multiple satellites is exploited in close proximity operations. Guidance and control algorithms are developed based on the closed-form analytical solution of relative motion equations that is completely explicit in time in a general Keplerian orbit. The guidance algorithm is based on a modified version of the inbound glideslope transfer that was used in the past for rendezvous and proximity operations of the space shuttle with other vehicles. The control algorithm is based on a discrete multipulse technique that was used to track the guidance trajectory efficiently while avoiding collisions between satellites during maneuvers. These algorithms are general, and can translate each satellite in the assembly in any direction and decelerate while approaching the desired target location in the final assembly configuration. Numerical nonlinear simulations that illustrate the performance and accuracy of the proposed algorithms are performed in a cubic formation assembly. Elsevier Masson SAS 2015-02 Article PeerReviewed application/pdf en http://irep.iium.edu.my/41283/1/1-s2.0-S1270963814002569-main.pdf Okasha, Mohamed Elsayed Aly Abd Elaziz and Park, Chandeok and Park, Sang-Young (2015) Guidance and control for satellite in-orbit-self-assembly proximity operations. Aerospace Science and Technology, 41. pp. 289-302. ISSN 1270-9638 E-ISSN 1626-3219 http://www.sciencedirect.com/science/article/pii/S1270963814002569 10.1016/j.ast.2014.11.011
repository_type Digital Repository
institution_category Local University
institution International Islamic University Malaysia
building IIUM Repository
collection Online Access
language English
topic TL500 Aeronautics
TL787 Astronautics
spellingShingle TL500 Aeronautics
TL787 Astronautics
Okasha, Mohamed Elsayed Aly Abd Elaziz
Park, Chandeok
Park, Sang-Young
Guidance and control for satellite in-orbit-self-assembly proximity operations
description In this paper, the autonomous in-orbit-self-assembly of multiple satellites is exploited in close proximity operations. Guidance and control algorithms are developed based on the closed-form analytical solution of relative motion equations that is completely explicit in time in a general Keplerian orbit. The guidance algorithm is based on a modified version of the inbound glideslope transfer that was used in the past for rendezvous and proximity operations of the space shuttle with other vehicles. The control algorithm is based on a discrete multipulse technique that was used to track the guidance trajectory efficiently while avoiding collisions between satellites during maneuvers. These algorithms are general, and can translate each satellite in the assembly in any direction and decelerate while approaching the desired target location in the final assembly configuration. Numerical nonlinear simulations that illustrate the performance and accuracy of the proposed algorithms are performed in a cubic formation assembly.
format Article
author Okasha, Mohamed Elsayed Aly Abd Elaziz
Park, Chandeok
Park, Sang-Young
author_facet Okasha, Mohamed Elsayed Aly Abd Elaziz
Park, Chandeok
Park, Sang-Young
author_sort Okasha, Mohamed Elsayed Aly Abd Elaziz
title Guidance and control for satellite in-orbit-self-assembly proximity operations
title_short Guidance and control for satellite in-orbit-self-assembly proximity operations
title_full Guidance and control for satellite in-orbit-self-assembly proximity operations
title_fullStr Guidance and control for satellite in-orbit-self-assembly proximity operations
title_full_unstemmed Guidance and control for satellite in-orbit-self-assembly proximity operations
title_sort guidance and control for satellite in-orbit-self-assembly proximity operations
publisher Elsevier Masson SAS
publishDate 2015
url http://irep.iium.edu.my/41283/
http://irep.iium.edu.my/41283/
http://irep.iium.edu.my/41283/
http://irep.iium.edu.my/41283/1/1-s2.0-S1270963814002569-main.pdf
first_indexed 2023-09-18T20:59:08Z
last_indexed 2023-09-18T20:59:08Z
_version_ 1777410505509437440

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