Comparison study of dynamic models for satellite formation flying
This thesis focuses on the comparison of dynamic models for satellite formation flying with the aid of simulation platforms Satellite Tool Kit (STK) and Matlab. One key challenge in formation flying technology is to model satellite relative dynamics. Based on the relative motion dynamic models, we c...
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sg-ntu-dr.10356-206552023-07-04T17:31:25Z Comparison study of dynamic models for satellite formation flying Hang, Yue Poh Eng Kee Wang Dan Wei School of Electrical and Electronic Engineering DRNTU::Engineering::Electrical and electronic engineering This thesis focuses on the comparison of dynamic models for satellite formation flying with the aid of simulation platforms Satellite Tool Kit (STK) and Matlab. One key challenge in formation flying technology is to model satellite relative dynamics. Based on the relative motion dynamic models, we can develop formation design and control strategies. Much work has been done concerning the relative motion of two satellites. In this thesis, firstly, a review is conducted on dynamic models of satellite formation flying. Then STK and Matlab will be used to evaluate the impact of different orbital perturbations on several linearized model. Later a model error index will be introduced to cornpare the accuracy of various dynamic models. Finally, the simulation results and analysis are presented. MASTER OF ENGINEERING (EEE) 2009-12-21T08:40:08Z 2009-12-21T08:40:08Z 2008 2008 Thesis Hang, Y. (2008). Comparison study of dynamic models for satellite formation flying. Master’s thesis, Nanyang Technological University, Singapore. https://hdl.handle.net/10356/20655 10.32657/10356/20655 en 84 p. application/pdf |
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DRNTU::Engineering::Electrical and electronic engineering Hang, Yue Comparison study of dynamic models for satellite formation flying |
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This thesis focuses on the comparison of dynamic models for satellite formation flying with the aid of simulation platforms Satellite Tool Kit (STK) and Matlab. One key challenge in formation flying technology is to model satellite relative dynamics. Based on the relative motion dynamic models, we can develop formation design and control strategies. Much work has been done concerning the relative motion of two satellites. In this thesis, firstly, a review is conducted on dynamic models of satellite formation flying. Then STK and Matlab will be used to evaluate the impact of different orbital perturbations on several linearized model. Later a model error index will be introduced to cornpare the accuracy of various dynamic models. Finally, the simulation results and analysis are presented. |
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Poh Eng Kee |
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Poh Eng Kee Hang, Yue |
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Theses and Dissertations |
author |
Hang, Yue |
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Hang, Yue |
title |
Comparison study of dynamic models for satellite formation flying |
title_short |
Comparison study of dynamic models for satellite formation flying |
title_full |
Comparison study of dynamic models for satellite formation flying |
title_fullStr |
Comparison study of dynamic models for satellite formation flying |
title_full_unstemmed |
Comparison study of dynamic models for satellite formation flying |
title_sort |
comparison study of dynamic models for satellite formation flying |
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2009 |
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https://hdl.handle.net/10356/20655 |
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1772828497184555008 |