Analytical Solutions of Atmospheric Drag Perturbation for Orbit Propagation

Description

Analytical solutions to the motion of the spacecraft subject to atmospheric drag, expressed in non-singular equinoctial orbital elements. The solutions are reported in a MATLAB file.

Date made available	10 Aug 2018
Publisher	University of Strathclyde

Contact

researchdataproject@strath.ac.uk

DOI
10.15129/63879118-7549-47ec-ad6e-bc6f77e0a6e5

Access Dataset

Integrals_Drag_Chebyshev3_2.m
File: text/plain, 64.5 KB
Type: Software
Licence: CC BY 4.0

1 Paper
1 Article

Automatic trajectory planning for low-thrust active removal mission in Low-Earth Orbit
Di Carlo, M., Romero Martin, J. M. & Vasile, M., 1 Mar 2017, In : Advances in Space Research. 59, 5, p. 1234-1258
Research output: Contribution to journal › Article

Open Access
File
14 Citations (Scopus)

43 Downloads (Pure)
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 Access
File

1 Finished

Astrium co-sponsored PhD on Low-thrust trajectory design
Vasile, M. & Macdonald, M.
Astrium Ltd
1/02/14 → 1/11/17
Project: Research - Studentship

Analytical Solutions of Atmospheric Drag Perturbation for Orbit Propagation

Description

Contact

DOI

Access Dataset

Automatic trajectory planning for low-thrust active removal mission in Low-Earth Orbit

Optimised GTO-GEO transfer using low-thrust propulsion

Astrium co-sponsored PhD on Low-thrust trajectory design

Cite this