Study of Stability of Equilibrium Points in The Pcr3bp on the Circumference of FEC

Author:

Vikash Kumar 1,Dr. K. B. Singh 2,Dr. M. N. Haque 3

Affiliation:

1. Research Scholar, University Department of Mathematics, B. R. A. Bihar University, Muzaffarpur, Bihar, India

2. P. G. Department of Physics, L. S. College, Muzaffarpur, B. R. A. Bihar University, Muzaffarpur, Bihar, India

3. P. G. Department of Mathematics, M. S. College, Motihari, B. R. A. Bihar University, Muzaffarpur, Bihar, India

Abstract

The Three Body Problem The three body problem studies the motion of three masses whose gravitational attraction have an effect on each other. The dynamics of the three-body problem are essentially different from those of two bodies, because in the latter case, an analytical solution may be found that admits orbits in the form of conic sections. This problem has been studied at great length and is the basis of most of today’s orbit planning and trajectory design for satellites. However, the two-body problem is valid on close to a single massive body, compared to which the target body (the object whose motion is desired) is essentially a massless particle. In deep space, when there may be two or more massive bodies to affect the motion of our test particle, the two-body solution obviously fails. It then becomes essential to study the three-body problem.

Publisher

Technoscience Academy

Subject

General Medicine

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