On some possible simplifications and changes in Hansen's lunar theory.
Hansen lunar theory extension, discussing applicability to satellites moving in orbits with high inclinations to sun orbital plane and Jovian satellites
Musen, P.↗
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On some possible simplifications and changes in Hansen's lunar theory.
Transforming Hansen lunar theory by referring satellite motion to almost ideal coordinate system, using general perturbations method
Musen, P.↗
On a modification of Hansen's lunar theory.
Modification of Hansens lunar theory to permit numerical treatment of solar perturbations of planetary satellites or of perturbations caused by the Earth
LUNAR SPACECRAFT↗
On some possible simplifications and changes in Hansen's lunar theory
Modifications and simplifications of Hansen lunar theory
Musen, P.↗
On the numerical theory of satellites with highly inclined orbits
Numerical lunar theory to obtain rectangular coordinates for satellite moving in highly inclined orbital plane - Hansen lunar theory
HANSEN LUNAR THEORY↗
The development of Hansen's coordinates in the lunar problem by the method of iteration
Computer program using Hansen lunar theory for calculating perturbations of lunar satellite
PERTURBATION↗
Application of Hansen's method to the 10th satellite of Jupiter
Application of Hansen lunar theory to 10th satellite of Jupiter
Charnow, M.↗
Computation of satellite orbits by the hansen method as modified by musen
Hansen theory of satellite orbit calculation as modified by musen
SATELLITE ORBIT↗
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↗
Differential correction of non-Keplerian reference orbits.
Differential correction vectors for non-Keplerian reference orbits, reexamining rotating ellipses in Hansen type intermediaries
STATE VECTOR↗
Development of the Lunar and Solar Perturbations in the Motion of an Artificial Satellite
Problems relating to the influence of lunar and solar perturbations on the motion of artificial satellites are analyzed by an extension of Cayley's development of the perturbative function in the lunar theory. In addition, the results are modified for incorporation into the Hansen-type theory used by the NASA Space Computing Center. The theory is applied to the orbits of the Vanguard I and Explorer VI satellites, and the results of detailed computations for these satellites are given together with a physical description of the perturbations in terms of resonance effects.
Musen, P.↗