A note on ?The main problem of satellite theory for small eccentricities, by A. Deprit and A. Rom, 1970?

Kaare Aksnes

doi:10.1007/bf01230328

A note on ?The main problem of satellite theory for small eccentricities, by A. Deprit and A. Rom, 1970?

Celestial Mechanics ◽

10.1007/bf01230328 ◽

1971 ◽

Vol 4 (1) ◽

pp. 119-121 ◽

Cited By ~ 13

Author(s):

Kaare Aksnes

Keyword(s):

Satellite Theory

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THE MAIN PROBLEM OF SATELLITE THEORY FOR SMALL ECCENTRICITIES

10.21236/ad0692617 ◽

1969 ◽

Cited By ~ 3

Author(s):

Andre Deprit ◽

Arnold Rom

Keyword(s):

Satellite Theory

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Second Order Solution of a Radial Intermediary in Satellite Theory

Astrophysics and Space Science Library - Space Dynamics and Celestial Mechanics ◽

10.1007/978-94-009-4732-0_23 ◽

1986 ◽

pp. 243-253 ◽

Cited By ~ 1

Author(s):

J. A. Caballero ◽

S. Ferrer ◽

M. L. Sein-Echaluce

Keyword(s):

Second Order ◽

Satellite Theory ◽

Order Solution

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Solution of the problem of artificial satellite theory without drag

The Astronomical Journal ◽

10.1086/107958 ◽

1959 ◽

Vol 64 ◽

pp. 378 ◽

Cited By ~ 552

Author(s):

Dirk Brouwer

Keyword(s):

Artificial Satellite ◽

Satellite Theory ◽

Artificial Satellite Theory

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Second-order solution of artificial satellite theory without air drag

The Astronomical Journal ◽

10.1086/108753 ◽

1962 ◽

Vol 67 ◽

pp. 446 ◽

Cited By ~ 103

Author(s):

Yoshibide Kozai

Keyword(s):

Artificial Satellite ◽

Second Order ◽

Satellite Theory ◽

Artificial Satellite Theory ◽

Air Drag ◽

Order Solution

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On the choice of reference orbit, canonical variables, and perturbation method in satellite theory

Celestial Mechanics ◽

10.1007/bf01231425 ◽

1973 ◽

Vol 8 (2) ◽

pp. 259-259 ◽

Cited By ~ 1

Author(s):

Kaare Aksnes

Keyword(s):

Perturbation Method ◽

Satellite Theory ◽

Reference Orbit ◽

Canonical Variables

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Application of Semi-analytical Satellite Theory orbit propagator to orbit determination for space object catalog maintenance

Advances in Space Research ◽

10.1016/j.asr.2016.02.028 ◽

2016 ◽

Vol 57 (10) ◽

pp. 2218-2233 ◽

Cited By ~ 8

Author(s):

Srinivas J. Setty ◽

Paul J. Cefola ◽

Oliver Montenbruck ◽

Hauke Fiedler

Keyword(s):

Orbit Determination ◽

Satellite Theory ◽

Space Object

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ATESAT: A symbolic processor for artificial satellite theory

Mathematics and Computers in Simulation ◽

10.1016/s0378-4754(97)00125-0 ◽

1998 ◽

Vol 45 (5-6) ◽

pp. 497-510 ◽

Cited By ~ 11

Author(s):

A. Abad ◽

A. Elipe ◽

J. Palacián ◽

J.F. San-Juan

Keyword(s):

Artificial Satellite ◽

Satellite Theory ◽

Artificial Satellite Theory

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The Stellar Problem of Three Bodies: I. Application of Satellite Theory

Monthly Notices of the Royal Astronomical Society ◽

10.1093/mnras/97.1.56 ◽

1936 ◽

Vol 97 (1) ◽

pp. 56-61 ◽

Cited By ~ 17

Author(s):

E. W. Brown

Keyword(s):

Satellite Theory

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Determination of mean elements for Vinti's satellite theory.

AIAA Journal ◽

10.2514/3.3532 ◽

1966 ◽

Vol 4 (4) ◽

pp. 740-741

Author(s):

N. L. BONAVITO

Keyword(s):

Satellite Theory ◽

Mean Elements

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Numerical integration of periodic orbits in the main problem of artificial satellite theory

Celestial Mechanics and Dynamical Astronomy ◽

10.1007/bf00695787 ◽

1994 ◽

Vol 58 (2) ◽

pp. 99-123 ◽

Cited By ~ 43

Author(s):

R. A. Broucke

Keyword(s):

Numerical Integration ◽

Periodic Orbits ◽

Artificial Satellite ◽

Satellite Theory ◽

Artificial Satellite Theory

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