Orbiter mission design problems
Planetary orbit design and selection for Mars orbiter mission
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Planetary orbit design and selection for Mars orbiter mission
Computational procedure for Vinti accurate reference orbit with inclusion of third zonal harmonic
Drift of inclined-orbit 24-hour satellite in earth gravity field through fourth order
Intermediate orbits of artificial earth satellite
System of state transition partial derivatives for which tracking information normal matrix for lunar orbiter is nearly diagonalized
Error bounds on position and velocity in satellite orbit theories
Space dynamics and control systems, spacecraft and subsystems, sensors, general electronics, environmental testing, tracking systems, and orbit determination
Orbital placement and control of Syncom-II SATELLITE
Perturbation technique to study three-body problem of motion of close satellite
Launch vehicle guidance, premidcourse orbit determination and midcourse maneuver of Ranger IX spacecraft lunar mission and merger
Atlas-Agena and Atlas-Centaur launch vehicles to investigate comets
Planet Mercury rotation theory, applying motion of rigid system in inverse square field
Tracking geometry and dynamics of lunar satellite, estimating orbital elements and lunar gravitational field parameters through Earth- based range and range rate observations
Classical spectroscopic binary star orbit determination techniques to provide orbital elements for lunar satellite tracked by Earth- based Doppler radar
Short-period Trojan orbits in restricted three- body problem numerically determined, using Jupiter and Sun as principal masses
Mean element determination for Vinti satellite theory
Classical spectroscopic binary star orbit determination techniques to provide orbital elements for lunar satellite tracked by Earth- based Doppler radar
Energy integral evaluation of higher-order terms in time history of satellite motion