Relative motion modeling and control in a perturbed orbit
In this paper, the dynamics of the relative motion problem in a perturbed orbital environment are exploited based on Gauss’ and Cowell’s variational equations. The inertial coordinate frame and relative coordinate frame (Hill frame) are studied to describe the relative motion. A linear high fidelit...
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| Format: | Proceeding Paper |
| Language: | en en |
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Univelt, Incorporated
2011
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| Online Access: | http://irep.iium.edu.my/38708/1/AAS_11-211.pdf http://irep.iium.edu.my/38708/4/Final_Program.pdf http://irep.iium.edu.my/38708/ http://www.univelt.com/book=2596 |
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| _version_ | 1834428880544333824 |
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| author | Okasha, Mohamed Elsayed Aly Abd Elaziz Newman, Brett |
| author_facet | Okasha, Mohamed Elsayed Aly Abd Elaziz Newman, Brett |
| author_sort | Okasha, Mohamed Elsayed Aly Abd Elaziz |
| building | IIUM Library |
| collection | Institutional Repository |
| content_provider | International Islamic University Malaysia |
| content_source | IIUM Repository (IREP) |
| continent | Asia |
| country | Malaysia |
| description | In this paper, the dynamics of the relative motion problem in a perturbed orbital environment are exploited based on Gauss’ and Cowell’s variational equations.
The inertial coordinate frame and relative coordinate frame (Hill frame) are studied to describe the relative motion. A linear high fidelity model is developed
to describe the relative motion. This model takes into account primary gravitational and atmospheric drag perturbations. In addition, this model is used in the
design of a control, guidance, and navigation system of a chaser vehicle to approach towards and to depart form a target vehicle in proximity operations. Relative
navigation uses an extended Kalman filter based on this relative model to estimate the relative position and velocity of the chaser vehicle with respect to
the target vehicle. This filter uses the range and angle measurements of the target relative to the chaser from a simulated LIDAR system. The corresponding measurement models, process noise matrix, and other filter parameters are provided. Numerical simulations are performed to assess the precision of this model with respect to the full nonlinear model. The analyses include the navigation errors and trajectory dispersions. |
| format | Proceeding Paper |
| id | my.iium.irep-38708 |
| institution | Universiti Islam Antarabangsa Malaysia |
| language | en en |
| publishDate | 2011 |
| publisher | Univelt, Incorporated |
| record_format | dspace |
| spelling | my.iium.irep-387082014-10-23T07:51:18Z http://irep.iium.edu.my/38708/ Relative motion modeling and control in a perturbed orbit Okasha, Mohamed Elsayed Aly Abd Elaziz Newman, Brett TL Motor vehicles. Aeronautics. Astronautics In this paper, the dynamics of the relative motion problem in a perturbed orbital environment are exploited based on Gauss’ and Cowell’s variational equations. The inertial coordinate frame and relative coordinate frame (Hill frame) are studied to describe the relative motion. A linear high fidelity model is developed to describe the relative motion. This model takes into account primary gravitational and atmospheric drag perturbations. In addition, this model is used in the design of a control, guidance, and navigation system of a chaser vehicle to approach towards and to depart form a target vehicle in proximity operations. Relative navigation uses an extended Kalman filter based on this relative model to estimate the relative position and velocity of the chaser vehicle with respect to the target vehicle. This filter uses the range and angle measurements of the target relative to the chaser from a simulated LIDAR system. The corresponding measurement models, process noise matrix, and other filter parameters are provided. Numerical simulations are performed to assess the precision of this model with respect to the full nonlinear model. The analyses include the navigation errors and trajectory dispersions. Univelt, Incorporated 2011-02 Proceeding Paper PeerReviewed application/pdf en http://irep.iium.edu.my/38708/1/AAS_11-211.pdf application/pdf en http://irep.iium.edu.my/38708/4/Final_Program.pdf Okasha, Mohamed Elsayed Aly Abd Elaziz and Newman, Brett (2011) Relative motion modeling and control in a perturbed orbit. In: 21st AAS/AIAA Space Flight Mechanics Meeting, 13–17 February 2011, New Orleans, Louisiana. http://www.univelt.com/book=2596 |
| spellingShingle | TL Motor vehicles. Aeronautics. Astronautics Okasha, Mohamed Elsayed Aly Abd Elaziz Newman, Brett Relative motion modeling and control in a perturbed orbit |
| title | Relative motion modeling and control in a perturbed orbit |
| title_full | Relative motion modeling and control in a perturbed orbit |
| title_fullStr | Relative motion modeling and control in a perturbed orbit |
| title_full_unstemmed | Relative motion modeling and control in a perturbed orbit |
| title_short | Relative motion modeling and control in a perturbed orbit |
| title_sort | relative motion modeling and control in a perturbed orbit |
| topic | TL Motor vehicles. Aeronautics. Astronautics |
| url | http://irep.iium.edu.my/38708/1/AAS_11-211.pdf http://irep.iium.edu.my/38708/4/Final_Program.pdf http://irep.iium.edu.my/38708/ http://www.univelt.com/book=2596 |
| url_provider | http://irep.iium.edu.my/ |