Computer Science
Scientific paper
Mar 1981
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1981kosis..19..165v&link_type=abstract
Kosmicheskie Issledovaniia, vol. 19, Mar.-Apr. 1981, p. 165-177. In Russian.
Computer Science
1
Circular Orbits, Eccentric Orbits, Orbit Calculation, Orbital Mechanics, Solar Orbits, Three Body Problem, Evolution (Development), Gauss Equation, Numerical Integration, Orbital Elements, Steady State
Scientific paper
A numerical-analytical method for determining the secular part of the disturbing function is used to calculate the limits of eccentricity variation of the evolving orbit of a zero-mass point in the framework of the restricted circular twice-averaged three body problem. Eccentricity values that correspond to the steady-state local solutions of the problem are determined. Two methods for calculating the evolution of asteroid-type orbits are compared: a method for solving the Gauss problem and a method of the numerical integration of rigorous equations of the restricted circular three body problem.
No associations
LandOfFree
Evolution of orbits in the restricted circular twice-averaged three body problem. II - Quantitative characteristics 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 Evolution of orbits in the restricted circular twice-averaged three body problem. II - Quantitative characteristics, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Evolution of orbits in the restricted circular twice-averaged three body problem. II - Quantitative characteristics will most certainly appreciate the feedback.
Profile ID: LFWR-SCP-O-1791406