Earth-mars trajectories, 1973, volume 5, part c
Machine computations of three-dimensional ballistic interplanetary trajectories - August and September 1973
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Machine computations of three-dimensional ballistic interplanetary trajectories - August and September 1973
Mariner IV trajectory analysis and importance of flight-path selection in construction of basic mission profile
Space mission trajectory optimization by iterative minimizing of residual vector, using linear correction
Steepest descent method to compute powered flight trajectory optimization for lunar and interplanetary transfer
Adaptive guidance correction policy developed from dynamic programming point of view for perturbed trajectory of spacecraft
Optimization of high thrust double-conic interplanetary trajectories - one-way planet- to-planet space flight
Analytical model for generation of earth-moon trajectory analysis data
Explicit equations for steering Atlas-Centaur multistage launch vehicle to lunar trajectory
Design parameters for ballistic interplanetary trajectories to Mercury and Jupiter
Space trajectories program for IBM 7090 computer
Earth-Moon trajectory mechanics analysis affected by geometric and booster vehicle considerations
Virtual Mass Technique for computing spacecraft trajectories and Fortran IV computer program for related restricted three-body problem
Interplanetary trajectory targeting technique with application to 1975 Venus flyby mission
Interplanetary trajectory computer program in Fortran for guidance and navigation studies
Trajectory analysis for Mars probe for entry from approach hyperbola or from Mars orbit
Spacecraft-comet rendezvous trajectory analyzed in terms of comet properties and spacecraft capabilities to determine feasibility of interception mission
Planetary entry trajectory control of manned vehicles for Earth and Mars atmospheres
Trajectory characteristics of high-thrust Mars missions and effect on other aspects of mission planning