Evolution of high-altitude earth-satellite orbits

Details Evolution of high-altitude earth-satellite orbits Evolution of high-altitude earth-satellite orbits

May 1987

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1987kosis..25..339v&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 25, May-June 1987, p. 339-355.

Computer Science

High Altitude, Orbit Calculation, Orbit Perturbation, Satellite Orbits, Solar Activity Effects, Temporal Distribution, Axes Of Rotation, Equations Of Motion, Lunar Effects

Scientific paper

Vashkoviak's (1986) numerical-analytical method is used to investigate the evolution of satellite orbits with semimajor axes of l00,000-200,000 km for time periods of 5-10 years. The results obtained with this method are compared with results of the numerical integration of rigorous equations of satellite motion with allowance for lunar and solar perturbation effects. The range of eccentricities and inclinations is determined for a 10-year period for initial almost-circular orbits with semimajor axes of 125,000 and 160,000 km.

Affiliated with

Also associated with

No associations

Rating

Evolution of high-altitude earth-satellite orbits 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 high-altitude earth-satellite orbits, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Evolution of high-altitude earth-satellite orbits will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-859077