Analytical solutions to the motion of the spacecraft subject to atmospheric drag, expressed in non-singular equinoctial orbital elements. The solutions are reported in a MATLAB file.
|Date made available||10 Aug 2018|
|Publisher||University of Strathclyde|
Di Carlo, M. (Creator), Vasile, M. (Creator) (10 Aug 2018). Analytical Solutions of Atmospheric Drag Perturbation for Orbit Propagation. University of Strathclyde. Integrals_Drag_Chebyshev3_2(.m). 10.15129/63879118-7549-47ec-ad6e-bc6f77e0a6e5