Optimum Exit Trajectories with Specified Transfer Angle
Keywords: Earth's gravitational field, Optimum trajectory
AbstractOptimum trajectory with specified transfer angle between two terminals in an inverse square gravitational field is investigated, criterion of optimization being minimum velocity increment at the initial terminal. Results are numerically illustrated for two orbits in Earth's gravitational field.
How to Cite
Srivastava, T., & Singh, M. (2014). Optimum Exit Trajectories with Specified Transfer Angle. Defence Science Journal, 19(1), 49-52. https://doi.org/10.14429/dsj.19.7467
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