The Envelope of a Family of Elliptic Orbits and Ballistic Trajectories

  • Евгений Иванович Бутиков SPbSU, St. Petersburg, Russia
Keywords: safety domain, Keplerian orbits, foci of the ellipse, elliptical mirror, ballistic trajectories

Abstract

The paper presents a simple geometric derivation for the “safety domain” boundary for the family of Keplerian orbits of satellites or ballistic missiles, moving in a central field of gravity, and for the family of parabolic trajectories of projectiles in a uniform gravitational field launched from a common starting point at equal velocities. Examples of practical application of the envelope of a family of orbits for solving ballistics problems are discussed. These examples are illustrated by computer simulations.

Author Biography

Евгений Иванович Бутиков, SPbSU, St. Petersburg, Russia

Eugene I. Butikov: Prof. at St.Petersburg State University

References

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Published
2017-06-03
How to Cite
Бутиков, Е. И. (2017). The Envelope of a Family of Elliptic Orbits and Ballistic Trajectories. Computer Tools in Education, (3), 50-56. Retrieved from http://cte.eltech.ru/ojs/index.php/kio/article/view/1401
Section
Computers in the teaching process