Satellite orbit calculations using geopotential coefficients up to high degree and order

Details Satellite orbit calculations using geopotential coefficients up to high degree and order Satellite orbit calculations using geopotential coefficients up to high degree and order

May 1994

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1994adspr..14...35w&link_type=abstract

Advances in Space Research, Volume 14, Issue 5, p. 35-42.

Computer Science

Scientific paper

First and higher order perturbations due to geopotential coefficients up to 360 degree and order are calculated using the analytical theory of artificial satellite motion. The theory is based on the geopotential expansion modified by introducing generalized lumped coefficients. The perturbations in the nonsingular orbital elements as well as in the components of the radius vector are calculated. The results for certain low satellite orbits obtained using 360 × 360 OSU91A gravity model are analysed. Precise calculations of geopotential perturbations as well as spectrums of perturbations for orbits of a few satellites (ERS-1, TOPEX) are analyzed using GEM-T2, GEM-T3 and GRIM4 models.

Affiliated with

Also associated with

No associations

Rating

Satellite orbit calculations using geopotential coefficients up to high degree and order 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 Satellite orbit calculations using geopotential coefficients up to high degree and order, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Satellite orbit calculations using geopotential coefficients up to high degree and order will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-884198