Progress in the elliptic restricted 3-body problem - Asteroids in the 2/1, 3/1, and 1/1 resonance

Details Progress in the elliptic restricted 3-body problem - Asteroids in the 2/1, 3/1, and 1/1 resonance Progress in the elliptic restricted 3-body problem - Asteroids in the 2/1, 3/1, and 1/1 resonance

Mar 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992cemda..54..195d&link_type=abstract

Celestial Mechanics and Dynamical Astronomy (ISSN 0923-2958), vol. 54, no. 1-3, p. 195-205.

Astronomy and Astrophysics

Astronomy

3

Elliptical Orbits, Lagrangian Equilibrium Points, Orbital Resonances (Celestial Mechanics), Three Body Problem, Asteroid Belts, Equations Of Motion, Jupiter (Planet), Jupiter Satellites

Scientific paper

Recent research on the elliptic restricted three-body problem concerning the motion of asteroids in the 2/1, 3/1, and 1/1 mean motion resonances with Jupiter is reviewed. Emphasis is placed on results more recent than 1988 derived numerically and analytically. Some of these asteroids originally in a gap can reach such high eccentricities that they can become Mars crossers, Jupiter crossers, and even earth crossers. New results on the largeness of stable zones around the Lagrangian equilibrium points L4 and L5 are presented and compared with existing ones.

Affiliated with

Also associated with

No associations

Rating

Progress in the elliptic restricted 3-body problem - Asteroids in the 2/1, 3/1, and 1/1 resonance does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.

If you have personal experience with Progress in the elliptic restricted 3-body problem - Asteroids in the 2/1, 3/1, and 1/1 resonance, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Progress in the elliptic restricted 3-body problem - Asteroids in the 2/1, 3/1, and 1/1 resonance will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-1215978