Impact of Non-gravitational Forces on Magellan Orbit Determination

A Historic Mission To Venus

Master Thesis (2018)
Author(s)

J.A. Inamdar (TU Delft - Aerospace Engineering)

Contributor(s)

Pieter N.A.M. Visser – Mentor

Dr. Daniel Arnold – Graduation committee member

Faculty
Aerospace Engineering
Copyright
© 2018 Jayraj Inamdar
More Info
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Publication Year
2018
Language
English
Copyright
© 2018 Jayraj Inamdar
Graduation Date
21-09-2018
Awarding Institution
Delft University of Technology
Project
['Venusian Gravity Field Recovery', 'Swiss-European Mobility Program']
Programme
['Aerospace Engineering']
Faculty
Aerospace Engineering
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Abstract

A detailed modeling of non-gravitational forces is an area that has been left unexplored in the past for orbit modeling of Magellan, primarily due to imperfect knowledge about its attitude and physical properties (optical properties and drag coefficient). As a result, past orbit analyses have restricted the non-gravitational force modeling by implementing a simple cannon-ball model for Magellan. Given that the Venusian surroundings can have significant impact on the spacecraft trajectory, the main objective of this project is to develop a reasonable macro-model for Magellan and investigate its impact on the modeled non-gravitational forces, and consequently on the orbit solution of the spacecraft. Presence of good non-gravitational force models can improve the dynamic orbit modeling of spacecraft, that can eventually enhance the gravity recovery capability of a mission.

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