POSITION AND VELOCITY PERTURBATIONS IN THE ORBITAL FRAME IN TERMS OF CLASSICAL ELEMENT PERTURBATIONS

被引：34

作者：

Casotto, Stefano ^{[1
]}

机构：

[1] Univ Texas Austin, Ctr Space Res, Austin, TX 78712 USA

来源：

CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY | 1993年 / 55卷 / 03期

关键词：

Satellite perturbations; radial; transverse; normal perturbations; two-body problem partials;

D O I：

10.1007/BF00692510

中图分类号：

P1 [天文学];

学科分类号：

0704 ;

摘要：

The transformation of classical orbit element perturbations to perturbations in position and velocity in the radial, transverse and normal directions of the orbital frame is developed. The formulation is given for the case of mean anomaly perturbations as well as for eccentric and true anomaly perturbations. Approximate formulas are also developed for the case of nearly circular orbits and compared with those found in the literature.

引用

页码：209 / 221

页数：13

共 16 条

[1]

[Anonymous], 1966, THEORY SATELLITE GEO

[2]

BROUCKE RA, 1970, ASTRON ASTROPHYS, V6, P173

[3] SOLUTION OF THE PROBLEM OF ARTIFICIAL SATELLITE THEORY WITHOUT DRAG [J].

BROUWER, D .

ASTRONOMICAL JOURNAL, 1959, 64 (09) :378-397

[4]

BROUWER D, 1961, METHODS CELESTICAL M

[5] OBSERVED TIDAL BRAKING IN THE EARTH MOON SUN SYSTEM [J].

CHRISTODOULIDIS, DC ;

SMITH, DE ;

WILLIAMSON, RG ;

KLOSKO, SM .

JOURNAL OF GEOPHYSICAL RESEARCH-SOLID EARTH AND PLANETS, 1988, 93 (B6) :6216-6236

[6]

ENGELIS T, 1987, 377 OH STAT U DEP GE

[7]

HERRICK WS, 1971, ASTRODYNAMICS, V2

[8] INFERENCE OF VARIATIONS IN THE GRAVITY-FIELD FROM SATELLITE-TO-SATELLITE RANGE RATE [J].

KAULA, WM .

JOURNAL OF GEOPHYSICAL RESEARCH, 1983, 88 (NB10) :8345-8349

[9]

Rosborough G. W., 1986, CSR861 U TEX AUST

[10] RADIAL, TRANSVERSE AND NORMAL SATELLITE POSITION PERTURBATIONS DUE TO THE GEOPOTENTIAL [J].

ROSBOROUGH, GW ;

TAPLEY, BD .

CELESTIAL MECHANICS, 1987, 40 (3-4) :409-421

← 1 2 →