For a stable circular orbit the centripetal acceleration is provided by the gravitational force and so we have,
For two orbits at r and
the relative angular velocity of one satellite with respect to the other is given by,
The above uses Taylor's expansion series. In other words the time taken for the satellites to come periodically approach their minimum distance is given by,
1 comment:
i like very much the way of ur solution and very anxious when the complte solution will be published
Post a Comment