Modeling and simulation of earth coverage of a low earth orbit (LEO) satellite
Abstract
Keywords
References
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Details
Primary Language
English
Subjects
Dynamics, Vibration and Vibration Control , Mechanical Engineering (Other)
Journal Section
Research Article
Authors
Murat Bakırcı
*
0000-0003-2092-1168
Türkiye
Early Pub Date
May 24, 2024
Publication Date
June 20, 2024
Submission Date
April 6, 2024
Acceptance Date
May 23, 2024
Published in Issue
Year 2024 Volume: 8 Number: 2
Cited By
Trajectory Linearisation of Relative Motion to Elliptical Orbit Target Using Tschauner–Hempel Equation
International Journal of Aeronautical and Space Sciences
https://doi.org/10.1007/s42405-025-00964-0