Artificial Triangular Points by Lorentz Force in the Restricted Three-Body Problem

The restricted three body problem was outlined. acceleration due to planetary magnetic field, in terms of space craft’s orbital elements, analysed. conditions for calculating the liberation points including mutual gravitational attraction and effect Lorentz were derived case circular planer bodies. stability solution artificial triangular studied. Finally, numerical investigation Sun-Jupiter system calculated as study. results show ability changing position by an order from 10−7 10−6 dimensionless x, y coordinates distance r Jupiter. This is equivalent about hundreds Kilometers which considerable.