A TECHNIQUE FOR OPTIMUM FINAL VALUE CONTROL OF POWERED FLIGHT TRAJECTORIES
Technique for controlling the acceleration vector along a powered flight trajectory using a linear perturbation method
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Technique for controlling the acceleration vector along a powered flight trajectory using a linear perturbation method
Variational calculus and computer logic for optimization of ascent trajectories and propellant loadings of multistage space vehicles
Nonlinear terminal guidance system for descent trajectories including soft landing
Calculus of variation methods used for trajectory optimization and guidance of rocket propelled vehicles
Earth-venus trajectories 1968-1969
Earth-venus trajectories 1968-1969
Earth parking orbits and free return circumlunar trajectories from launch windows with fixed azimuths - apollo project
Mars nonstop round-trip trajectories using gravity supplemented by propulsion or aerodynamic forces
Energy-optimal trajectories for terminal phase of satellite rendezvous
Powered-descent trajectory for lunar landing mission of lunar excursion module
Booster parametric design method for performance and trajectory analysis - propulsion
Numerical techniques for trajectory optimization discussing steepest descent, second variation and generalized newton-raphson methods
Steepest descent, second variation and generalized newton-raphson trajectory optimization techniques applied to minimum time, low thrust, circle-to- circle transfer problems
Moon to earth trajectory analysis using conical section theory and precision integrating programs
Factors affecting free return circumlunar trajectories from launch windows with fixed launch azimuths, emphasizing effects of parking orbit launch time
Generalized precision trajectory program for ranger lunar and mariner interplanetary missions
Determination of spacecraft orbits by trajectory measurement data