Peloni, A. , McInnes, C. R. and Ceriotti, M. (2018) Osculating Keplerian elements for highly non-Keplerian orbits. Journal of Guidance, Control, and Dynamics, 41(11), pp. 2489-2498. (doi: 10.2514/1.G002867)
|
Text
163595.pdf - Accepted Version 956kB |
Abstract
No abstract available.
| Item Type: | Articles |
|---|---|
| Additional Information: | The content of this paper was presented at the 27th AAS/AIAA Space Flight Mechanics Meeting held in San Antonio, TX, USA on February, 5-9 2017. AAS Paper 17-278. http://eprints.gla.ac.uk/136992/ |
| Status: | Published |
| Refereed: | Yes |
| Glasgow Author(s) Enlighten ID: | Ceriotti, Dr Matteo and Peloni, Mr Alessandro and McInnes, Professor Colin |
| Authors: | Peloni, A., McInnes, C. R., and Ceriotti, M. |
| College/School: | College of Science and Engineering > School of Engineering College of Science and Engineering > School of Engineering > Systems Power and Energy |
| Journal Name: | Journal of Guidance, Control, and Dynamics |
| Publisher: | American Institute of Aeronautics and Astronautics |
| ISSN: | 0731-5090 |
| ISSN (Online): | 1533-3884 |
| Published Online: | 30 August 2018 |
| Copyright Holders: | Copyright © 2018 The Authors |
| First Published: | First published in Journal of Guidance, Control, and Dynamics 41(11):2489-2498 |
| Publisher Policy: | Reproduced in accordance with the copyright policy of the publisher |
University Staff: Request a correction | Enlighten Editors: Update this record
Funder and Project Information
Funder and Project Information