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
Engineering topics
Publications and source records attributed to Musen, P..
Numerical lunar theory to obtain rectangular coordinates for satellite moving in highly inclined orbital plane - Hansen lunar theory
Perturbations of position vector of planetary system
Lunar and solar long period effects on motion and orbit stability of satellites
Long period lunar and solar effects on motion of artificial satellite
Long period perturbation effects on satellite motion by ellipticity of earth equator
Orbital mechanics, examining problems relating to patched conics, perigee determination, eccentricity of satellite orbits and drag effect computations
Semianalytical theory of general planetary perturbations - Hill method
Development of a new theory of general planetary perturbations in rectangular coordinates
Modification of Hansens lunar theory to permit numerical treatment of solar perturbations of planetary satellites or of perturbations caused by the Earth
Numerical integration of long-range lunar effects in the motion of artificial satellites by extension of halperns method of secular perturbations
Perturbations of the motion of a 24-hr satellite which are caused by earths ellipticity at the equator, calculated, using bohlin resonance theory
Applicability of halphen method to computing long- range effects in motion of celestial bodies on artificial satellites
Halphen method and a resonance theory for determining long range effects of moon, sun and earth gravitational field irregularity in motion of artificial satellites
Combination of Halphen and Liouville methods for determining secular and critical effects in satellite orbit behavior
General planetary perturbations in rectangular coordinates
Series expansion of spherical functions for position perturbation theory of planetary system