Kinematics of tight transition of asteroid near Earth and it withdrawal in elementary sense
UDC
629.78.001.5:523.44Abstract
Article discusses about the problem of withdrawal asteroid by change the parameter pass, forming a new orbit, safe for subsequent long period of time. It is shown that a minimum distance of withdrawal as a control parameter gravity manoeuvre in the linear approach is completely defined by two vectors: geocentric velocity vector of the asteroid, and the vector of the targeting point, a given change in the current coordinates of the asteroid's approach and serves to correct the orbit.
Keywords:
asteroids, asteroid threatReferences
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Copyright (c) 2013 Pol V.G., Simonov A.V.
This work is licensed under a Creative Commons Attribution 4.0 International License.
