Tumbling motions of an artificial satellite.
Motion of passively damped gravity-stabilized artificial satellite tumbling or rotating about arbitrary axis
PERTURBATION THEORY↗
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Improvement of the spheroidal method for artificial satellites
Spheroidal method for calculating polar orbits of artificial satellites
Vinti, J. P.↗
Methods of averages expansions for artificial satellite applications
Formulas derived for averaged potential in artificial satellite theory
Liu, A.↗
Measurement of proton spectra on satellites from the Cosmos series of artificial satellites
In 1966-1967 measurements were performed at altitudes from 200 to 400 km to determine the fluxes and spectra of protons by means of nuclear emulsions of the BR-2 and Ya-2 types. The proton spectra within the range up to 8 BeV are presented. The spectra obtained are the basis for estimating radiation hazards.
Kovalev, Y. Y.↗
Determination of orbits of planetary artificial satellites and planetary gravitational fields
Orbit determination of planetary artificial satellites and planetary gravitational fields
Greer, C. L.↗
A second-order artificial satellite theory based on an intermediate orbit
Second order artificial satellite theory based on intermediate orbit
Aksnes, K.↗
A second-order artificial satellite theory based on an intermediate orbit
Oblate planet artificial satellite motion, obtaining secular and periodic perturbations to third and second order
Aksnes, K.↗
A unified treatment of lunar theory and artificial satellite theory
Generalized von Zeipel treatment of lunar and artificial satellite theories, generating single canonical transformation by variable separation technique
Mersman, W. A.↗
COMPARISON OF THE VON ZEIPEL AND MODIFIED HANSEN METHODS AS APPLIED TO ARTIFICIAL SATELLITES
Application of von zeipel and modified hansen methods to artificial satellite orbit calculations
VON ZEIPEL METHOD↗
Motion of an artificial satellite under combined influence of planar and Keplerian force fields
Artificial satellite motion under influence of planar and Keplerian force fields
Burns, R. E.↗
The equations of motion of an artificial satellite in nonsingular variables
The equations of motion of an artificial satellite are given in nonsingular variables. Any term in the geopotential is considered as well as luni-solar perturbations up to an arbitrary power of r/r prime; r prime being the geocentric distance of the disturbing body. Resonances with tesseral harmonics and with the moon or sun are also considered. By neglecting the shadow effect, the disturbing function for solar radiation is also developed in nonsingular variables for the long periodic perturbations. Formulas are developed for implementation of the theory in actual computations.
Giacaglia, G. E. O.↗
The equations of motion of an artificial satellite in nonsingular variables
The equations of motion of an artificial satellite are given in nonsingular variables. Any term in the geopotential is considered as well as luni-solar perturbations up to an arbitrary power of r/r', r' being the geocentric distance of the disturbing body. Resonances with tesseral harmonics and with the moon or sun are also considered. By neglecting the shadow effect, the disturbing function for solar radiation is also developed in nonsingular variables for the long periodic perturbations. Formulas are developed for implementation of the theory in actual computations.
Giacaglia, G. E. O.↗
On the long-period lunar and solar effects on the motion of an artificial satellite, 2
Long period lunar and solar effects on motion of artificial satellite
SATELLITE ORBIT↗
Inclusion of the third zonal harmonic in an accurate reference orbit of an artificial satellite.
Inclusion of third zonal harmonic in accurate reference orbit of artificial satellite
ZONAL HARMONICS↗
Short period lunar and solar perturbations for artificial satellites
Tabulated expressions of short period lunar and solar perturbations for artificial satellites
TABLE↗
Orbital prediction and differential correction using Vinti's spheroidal theory for artificial satellites
Orbital prediction and differential correction using Vintis spheroidal theory for artificial satellites
SATELLITE ORBIT↗
A feasibility study of determining physical properties of the Martian atmosphere by use of solar occultation as seen from an artificial satellite
Physical properties of Martian atmosphere using solar occultation seen from artificial satellite
Wallio, H. A.↗