Analytical Method for Calculating the Trajectories of Spacecraft Executing Dynamic Thrust Maneuvers and Orbit Corrections
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Using analytical methods is an efficient approach to qualitative analysis of spacecraft (SC) trajectories. An analytical method is described of calculating the parameters of SC motion during dynamic thrust maneuvers and corrections with the account of aerodynamic forces affecting the SC. Computational margins are analyzed of calculating the parameters of SC motion. Full qualitative agreement between the data retrieved and the results of numerical integration of differential equations yields a computational error margin within just 2–3%.
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