Abstract
The present work is devoted to theEarth’s protection from asteroid danger, namely, the use of the kinetic interceptor - a spacecraft, which by means of collision repels an asteroid from a dangerous orbit. The parameters of near-Earth asteroids are revealed. Mathematical model of the control movement of all bodies (the Earth, the Sun, the asteroid, the spacecraft), the control program and software package (Delphi 7) for the simulation and visualization of the trajectories are designed.
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