Research output per year
Research output per year
Description
Analytical solutions to the motion of the spacecraft subject to J3, J4, J5 and third body perturbations, expressed in non-singular equinoctial orbital elements. The solutions are reported in MATLAB files.
Data to be made public at the discretion of the data creator.
Data to be made public at the discretion of the data creator.
| Date made available | 10 Aug 2018 |
|---|---|
| Publisher | University of Strathclyde |
Research output
- 1 Paper
-
Optimised GTO-GEO transfer using low-thrust propulsion
Di Carlo, M., Vasile, M. & Kemble, S., 3 Jun 2017. 10 p.Research output: Contribution to conference › Paper
Open AccessFile
Projects
- 1 Finished
-
Astrium co-sponsored PhD on Low-thrust trajectory design
1/02/14 → 1/11/17
Project: Research - Studentship