Parametric optimization of near-equatorial twin-spacecrafts trajectory based on ground-track performance measure requirements.
Parametric optimization study is carried out on Performance Measure for assessing the benefits of relevant ground-track parameters and Instantaneous Overlap Area (IOA) in near earth and near-equatorial twin-satellite formation flying to explore its potential for of spacecraft formation flying as spa...
| Main Authors: | , |
|---|---|
| Format: | Conference or Workshop Item |
| Language: | English English |
| Published: |
2012
|
| Online Access: | http://psasir.upm.edu.my/id/eprint/27766/ http://psasir.upm.edu.my/id/eprint/27766/1/ID%2027766.pdf |
| _version_ | 1848845931169972224 |
|---|---|
| author | Djojodihardjo, Harijono A.Gunter, A. Aq'Grabin |
| author_facet | Djojodihardjo, Harijono A.Gunter, A. Aq'Grabin |
| author_sort | Djojodihardjo, Harijono |
| building | UPM Institutional Repository |
| collection | Online Access |
| description | Parametric optimization study is carried out on Performance Measure for assessing the benefits of relevant ground-track parameters and Instantaneous Overlap Area (IOA) in near earth and near-equatorial twin-satellite formation flying to explore its potential for of spacecraft formation flying as space platform to carry out Tropical Resources and Environment Monitoring mission. The present study also emphasizes two aspects: the dynamics of relative motion
of multiple spacecrafts and the desirable ground tracks beneficial for tropical environmental and resources monitoring missions. Relative motion dynamics incorporating Clohessy-Wiltshire Equation for circular orbits is used as a
reference. Related to the relevance of Ground-Track based characteristics and to optimize computational efforts, the performance metric is synthesized as a off between exact definition and intuitive judgment. |
| first_indexed | 2025-11-15T08:54:39Z |
| format | Conference or Workshop Item |
| id | upm-27766 |
| institution | Universiti Putra Malaysia |
| institution_category | Local University |
| language | English English |
| last_indexed | 2025-11-15T08:54:39Z |
| publishDate | 2012 |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | upm-277662014-06-20T01:04:59Z http://psasir.upm.edu.my/id/eprint/27766/ Parametric optimization of near-equatorial twin-spacecrafts trajectory based on ground-track performance measure requirements. Djojodihardjo, Harijono A.Gunter, A. Aq'Grabin Parametric optimization study is carried out on Performance Measure for assessing the benefits of relevant ground-track parameters and Instantaneous Overlap Area (IOA) in near earth and near-equatorial twin-satellite formation flying to explore its potential for of spacecraft formation flying as space platform to carry out Tropical Resources and Environment Monitoring mission. The present study also emphasizes two aspects: the dynamics of relative motion of multiple spacecrafts and the desirable ground tracks beneficial for tropical environmental and resources monitoring missions. Relative motion dynamics incorporating Clohessy-Wiltshire Equation for circular orbits is used as a reference. Related to the relevance of Ground-Track based characteristics and to optimize computational efforts, the performance metric is synthesized as a off between exact definition and intuitive judgment. 2012 Conference or Workshop Item PeerReviewed application/pdf en http://psasir.upm.edu.my/id/eprint/27766/1/ID%2027766.pdf Djojodihardjo, Harijono and A.Gunter, A. Aq'Grabin (2012) Parametric optimization of near-equatorial twin-spacecrafts trajectory based on ground-track performance measure requirements. In: First IAA-AAS Conference on Dynamic & Control of Space System 2012 , 19-23 Mar. 2012, California, USA . (pp. 1-16). English |
| spellingShingle | Djojodihardjo, Harijono A.Gunter, A. Aq'Grabin Parametric optimization of near-equatorial twin-spacecrafts trajectory based on ground-track performance measure requirements. |
| title | Parametric optimization of near-equatorial twin-spacecrafts trajectory based on ground-track performance measure requirements. |
| title_full | Parametric optimization of near-equatorial twin-spacecrafts trajectory based on ground-track performance measure requirements. |
| title_fullStr | Parametric optimization of near-equatorial twin-spacecrafts trajectory based on ground-track performance measure requirements. |
| title_full_unstemmed | Parametric optimization of near-equatorial twin-spacecrafts trajectory based on ground-track performance measure requirements. |
| title_short | Parametric optimization of near-equatorial twin-spacecrafts trajectory based on ground-track performance measure requirements. |
| title_sort | parametric optimization of near-equatorial twin-spacecrafts trajectory based on ground-track performance measure requirements. |
| url | http://psasir.upm.edu.my/id/eprint/27766/ http://psasir.upm.edu.my/id/eprint/27766/1/ID%2027766.pdf |