Optimal Trajectory Synthesis for Spacecraft Asteroid Rendezvous
Several researchers are considering the plausibility of being able to rapidly launch a mission to an asteroid, which would fly in close proximity of the asteroid to deliver an impulse in a particular direction so as to deflect the asteroid from its current orbit. Planetary motion, in general, and th...
Main Authors: | Ranjan Vepa, M. Hasan Shaheed |
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Format: | Article |
Language: | English |
Published: |
MDPI AG
2021-08-01
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Series: | Symmetry |
Subjects: | |
Online Access: | https://www.mdpi.com/2073-8994/13/8/1403 |
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