Semi-analytical attitude propagation for earth orbiting objects
Cavallari, I. and Feng, J. and Vasile, M. (2025) Semi-analytical attitude propagation for earth orbiting objects. Communications in Nonlinear Science and Numerical Simulation, 142. 108549. ISSN 1007-5704 (https://doi.org/10.1016/j.cnsns.2024.108549)
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Abstract
This paper presents the development of a semi-analytical theory for the long-term propagation of the attitude motion of Earth-orbiting objects with arbitrary shape. The attitude dynamics includes the effects of gravity-gradient, residual magnetic, and light-pressure torques. The equations of motion are expressed in Sadov variables. The equations of motion are averaged over the Sadov angles and the orbital mean anomaly and a combination of Lie transformations is applied to transform from non-averaged to mean attitude variables. It will be shown how this technique can be used to estimate the approximation error and improve the accuracy of the averaged solution. Furthermore, we introduce an alternative set of variables, that removes one of the singularities in the formulation in Sadov variables. The results of the numerical tests demonstrate that the proposed semi-analytical theory, provides a good balance between accuracy and computational cost.
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: 91859 Dates: DateEvent1 March 2025Published30 December 2024Published Online13 December 2024Accepted1 May 2024SubmittedSubjects: 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: 22 Jan 2025 11:03 Last modified: 22 Jan 2025 11:04 URI: https://strathprints.strath.ac.uk/id/eprint/91859