Method and device management trajectory of the cosmic body inertial influence of movement

摘要

1. A method for controlling the trajectory of movement of outer body (CT) (asteroid, comets, satellites or missiles parts) by inertial impact onto the surface of RT blocks arrive spacecraft using auxiliary means of communication and navigation, characterized in that the blocks are placed in one or more, inertial propulsion devices, such as magnetoelectric inertial propulsion (MEID), shipping blocks MEID CT performed alternately of spacecraft (SC), positioned in space, and not through necessity intervals of time, at the approach to CT, blocks with MEID is lowered to the surface on the pitch oriented relative to the path CT motion inertial propulsion affect the CT at the point of landing on its surface, corresponding to the passage path, e.g., through the center CT of the masses, wherein commands to the gyro orientation and the axial propulsors inertial effects of the first block and subsequent blocks is performed after attaching them onto the surface of RT, with the remaining blocks inertial propulsion alternately nap ulation, in accordance with the received information, and using spacecraft (SC) control, the results of said effects on natural trajectory CT movements make the transition to a predetermined, controlled trajectory and retention of this trajectory, by planting additional inertial units, in the final step movement by a spacecraft in Earth transmit information on the RT retention on this trajectory, then, and, if necessary, control the movement CT alter trajectory and directed at RT