Application of Hamilton Principle in the control of Tethered Satellite System Pendular Motion

The control of a tethered satellite system pendular motion is done by application of Hamiltonian equation of motion on a control design method known as planar H tracking. In this case, the reference motion is considered a natural planar motion. The control of the TSS is accomplished by using the ins...

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Main Authors: Paul TIROP, Zhang JINGRUI
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2018-06-01
Series:INCAS Bulletin
Subjects:
Online Access:http://bulletin.incas.ro/files/tirop_jingrui_vol_10_iss_2.pdf
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author Paul TIROP
Zhang JINGRUI
author_facet Paul TIROP
Zhang JINGRUI
author_sort Paul TIROP
collection DOAJ
description The control of a tethered satellite system pendular motion is done by application of Hamiltonian equation of motion on a control design method known as planar H tracking. In this case, the reference motion is considered a natural planar motion. The control of the TSS is accomplished by using the inside plane control inputs as well as the outside plane control inputs. The designed control laws are able to drive the pendular motion to a natural planar trajectory with the required characteristics. The control inputs are analyzed using their magnitude ability. The numerical simulation results for each control inputs show that the inside of plane input not only has strong magnitude, but also effectively controls the pendular motion of the tethered satellite system.
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spelling doaj.art-a4a19553b6e9429b93e8c55be6e58d372022-12-22T03:16:03ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282018-06-011029911010.13111/2066-8201.2018.10.2.10Application of Hamilton Principle in the control of Tethered Satellite System Pendular MotionPaul TIROP0Zhang JINGRUI1Beijing Institute of Technology, No. 5 Zhongguancun Street, Haidian District, Beijing, 100081, China, paultirop@yahoo.com*Beijing Institute of Technology, No. 5 Zhongguancun Street, Haidian District, Beijing, 100081, China, zhangjingrui@bit.edu.cnThe control of a tethered satellite system pendular motion is done by application of Hamiltonian equation of motion on a control design method known as planar H tracking. In this case, the reference motion is considered a natural planar motion. The control of the TSS is accomplished by using the inside plane control inputs as well as the outside plane control inputs. The designed control laws are able to drive the pendular motion to a natural planar trajectory with the required characteristics. The control inputs are analyzed using their magnitude ability. The numerical simulation results for each control inputs show that the inside of plane input not only has strong magnitude, but also effectively controls the pendular motion of the tethered satellite system.http://bulletin.incas.ro/files/tirop_jingrui_vol_10_iss_2.pdfTethered Satellite SystemHamiltonian equationControl lawsPendular motion
spellingShingle Paul TIROP
Zhang JINGRUI
Application of Hamilton Principle in the control of Tethered Satellite System Pendular Motion
INCAS Bulletin
Tethered Satellite System
Hamiltonian equation
Control laws
Pendular motion
title Application of Hamilton Principle in the control of Tethered Satellite System Pendular Motion
title_full Application of Hamilton Principle in the control of Tethered Satellite System Pendular Motion
title_fullStr Application of Hamilton Principle in the control of Tethered Satellite System Pendular Motion
title_full_unstemmed Application of Hamilton Principle in the control of Tethered Satellite System Pendular Motion
title_short Application of Hamilton Principle in the control of Tethered Satellite System Pendular Motion
title_sort application of hamilton principle in the control of tethered satellite system pendular motion
topic Tethered Satellite System
Hamiltonian equation
Control laws
Pendular motion
url http://bulletin.incas.ro/files/tirop_jingrui_vol_10_iss_2.pdf
work_keys_str_mv AT paultirop applicationofhamiltonprincipleinthecontroloftetheredsatellitesystempendularmotion
AT zhangjingrui applicationofhamiltonprincipleinthecontroloftetheredsatellitesystempendularmotion