Optimum Exit Trajectories with Specified Transfer Angle

Authors

  • T. N. Srivastava Defence Science Laboratory, Delhi
  • M. Singh Defence Science Laboratory, Delhi

DOI:

https://doi.org/10.14429/dsj.19.7467

Keywords:

Earth's gravitational field, Optimum trajectory

Abstract

Optimum 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.

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Published

2014-05-23

How to Cite

Srivastava, T. N., & 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

Issue

Vol. 19 No. 1

Section

Research Papers

License

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