Date of Award
Fall 12-2020
Document Type
Thesis
Degree Name
Master of Science (MS)
Department
Mechanical & Aerospace Engineering
Program/Concentration
Aerospace Engineering
Committee Director
Brett Newman
Committee Member
Robert Ash
Committee Member
Sharan Asundi
Committee Member
Dimitrie Popescu
Abstract
Simple orbital maneuvers obeying Kepler’s Laws, when taken with respect to Newton’s framework, require considerable time and effort to interpret and understand. Instead of a purely mathematical approach relying on the governing relations, a graphical geometric conceptual representation provides a useful alternative to the physical realities of orbits. Conic sections utilized within the full scope of a modified cone (frustum) were employed to demonstrate and develop a geometric approach to elliptical orbit transformations. The geometric model in-question utilizes the rotation of a plane intersecting the orbital frustum at some angle β (and the change in this angle) in a novel approach to analyze and develop two-body elliptical orbital transformations. Beginning with simple algebraic concepts such as Newton’s Second Law and the total specific orbital energy equation, equations combining two-body concepts with more general, Newtonian physics are explored; several equations relating eccentricity directly to a change in orbital energy are developed and applied; and conclusions regarding their importance and usefulness are drawn. Orbital energy exchange, eccentricity, and orbital shape from both inertial and non-inertial perspectives have been developed. Visualizations of transformations are presented throughout to aid in comprehension and clarity. Finally, efficacy of the model, extensions to non-stable orbits, and accuracy and precision with example calculations have been outlined in the Appendices.
Rights
In Copyright. URI: http://rightsstatements.org/vocab/InC/1.0/ This Item is protected by copyright and/or related rights. You are free to use this Item in any way that is permitted by the copyright and related rights legislation that applies to your use. For other uses you need to obtain permission from the rights-holder(s).
DOI
10.25777/vnvw-af67
ISBN
9798557057219
Recommended Citation
Branco, Cian A..
"Conical Orbital Mechanics: A Rework of Classic Orbit Transfer Mechanics"
(2020). Master of Science (MS), Thesis, Mechanical & Aerospace Engineering, Old Dominion University, DOI: 10.25777/vnvw-af67
https://digitalcommons.odu.edu/mae_etds/329
Included in
Aerospace Engineering Commons, Applied Mathematics Commons, Mechanical Engineering Commons