Methods of averages expansions for artificial satellite applications
Formulas derived for averaged potential in artificial satellite theory
Engineering topics
Publications and source records attributed to Lorell, J..
Formulas derived for averaged potential in artificial satellite theory
Lunar Orbiter tracking data for long term selenodesy
Moon gravity field model derived from long-arc analysis of Lunar Orbiters tracking data, considering lunar mass distribution role
Celestial mechanics experiment for Mariner Mars 1971 to test general relativity theory and improve Martian ephemeris
Lunar gravity estimates using tracking data from lunar orbiters, including tesseral and zonal harmonic coefficients
Large Doppler residuals near pericynthion found in lunar orbiter tracking data
Gravity data from lunar orbiter tracking, discussing Kepler element role
Application of double-averaged equations of artificial satellite motion to lunar orbiter
Third-body perturbation effects on satellite orbit reduced to nonlinear system requiring elliptic integrals
Long term time-variation of osculating elements of satellite orbits perturbed by third body, including graphs of Kepler element variations along different orbits
Characteristics and format of tracking data to be obtained by Deep Space Instrumentation Facility /DSIF/ for lunar orbiter
Lunar satellite orbit determination, using doppler data, optical data and range and range rate data
Long period component and secular component of satellite motion evaluated, using lagrange planetary equation
Perturbation analysis of the general theory of relativity and development of variations in the two-body keplarian orbital elements /see accession no. a63-15324, issue no. 11/
Perturbation analysis of the general theory of relativity and development of variations in the two-body keplerian orbital elements
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