The effects of solar radiation pressure on the motion of an artificial satellite

Abstract

This thesis documents an investigation of the effect of solar radiation pressure on the motion of an artificial satellite. Consideration is given to the methods required for the inclusion of the discontinuous effect of the Earth's shadow. The analysis resulting from the description of a deformed diffusely reflecting balloon satellite and an algorithm describing the effects of Earth reflected solar radiation pressure are developed, culminating in the application of the derived theory to the orbital data of the balloon satellite, Explorer 19.

Divisions: College of Engineering & Physical Sciences
Additional Information: Department: Satellite Tracking Unit If you have discovered material in Aston Research Explorer which is unlawful e.g. breaches copyright, (either yours or that of a third party) or any other law, including but not limited to those relating to patent, trademark, confidentiality, data protection, obscenity, defamation, libel, then please read our Takedown policy and contact the service immediately (openaccess@aston.ac.uk)
Institution: Aston University
Uncontrolled Keywords: satellite,orbit,perturbation,solar radiation
Last Modified: 30 Sep 2024 07:29
Date Deposited: 21 Feb 2011 11:03
Completed Date: 1979
Authors: Ryland, Frederick C.E.

Download

Export / Share Citation


Statistics

Additional statistics for this record