Euler-Newton-type differential equations for osculating Eulerian elements

Details Euler-Newton-type differential equations for osculating Eulerian elements Euler-Newton-type differential equations for osculating Eulerian elements

Feb 1989

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989azh....66..161t&link_type=abstract

Astronomicheskii Zhurnal (ISSN 0004-6299), vol. 66, Jan.-Feb. 1989, p. 161-171. In Russian.

Astronomy and Astrophysics

Astronomy

1

Astrodynamics, Celestial Mechanics, Euler Equations Of Motion, Satellite Orbits, Differential Equations, Newton Theory, Oblate Spheroids, Satellite Perturbation

Scientific paper

Euler-Newton-type differential equations are obtained for the a, e, s, l, g, and h elements of the satellite's intermediate orbit. An asymmetrical variant of the Eulerian orbit was used as the intermediate one. The coefficients of the components of the perturbing acceleration are represented in the equations with an accuracy up to the terms proportional to parameters having the order of the oblateness of the earth.

Affiliated with

Also associated with

No associations

Rating

Euler-Newton-type differential equations for osculating Eulerian elements 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 Euler-Newton-type differential equations for osculating Eulerian elements, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Euler-Newton-type differential equations for osculating Eulerian elements will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-1884478