Semi-analytical attitude propagation of low-altitude Earth orbiting objects
Cavallari, I. and Feng, J. and Vasile, M. (2025) Semi-analytical attitude propagation of low-altitude Earth orbiting objects. Communications in Nonlinear Science and Numerical Simulation, 142. 108550. ISSN 1007-5704 (https://doi.org/10.1016/j.cnsns.2024.108550)
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Abstract
The paper introduces an averaged model suitable for studying the long-term attitude dynamics of low Earth orbit objects subject to the interaction with the exosphere. This work extends previous results by the authors on the development of a semi-analytical theory for long-term attitude propagation. The first-order averaged model is developed by expressing the rotational problem in modified Sadov variables and performing the average of the equations of motion over the fast Sadov angles and the orbital mean anomaly. A transformation from osculating to mean variables is also derived from a combination of Lie transformations. The approach proposed in this paper is applied to two possible atmospheric drag models: a simple, commonly used, model characterised by a constant dimensionless drag coefficient and a higher fidelity model based on the theory by Sentman (1961).
ORCID iDs
Cavallari, I., Feng, J. ORCID: https://orcid.org/0000-0003-0376-886X and Vasile, M. ORCID: https://orcid.org/0000-0001-8302-6465;-
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Item type: Article ID code: 91639 Dates: DateEvent31 March 2025Published30 December 2024Published Online13 December 2024AcceptedSubjects: Technology > Motor vehicles. Aeronautics. Astronautics > Aeronautics. Aeronautical engineering Department: Faculty of Engineering > Mechanical and Aerospace Engineering
Strategic Research Themes > Ocean, Air and Space
Technology and Innovation Centre > Advanced Engineering and ManufacturingDepositing user: Pure Administrator Date deposited: 20 Dec 2024 13:22 Last modified: 10 Jan 2025 11:26 URI: https://strathprints.strath.ac.uk/id/eprint/91639