AN APPLICATION OF A SUCCESSIVE APPROXIMATION SCHEME TO OPTIMIZING VERY LOW-THRUST TRAJECTORIES
Spacecraft guidance - low thrust propulsion trajectories
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Spacecraft guidance - low thrust propulsion trajectories
Control of acceleration vector of powered flight trajectory
Low thrust propulsion interplanetary trajectory flight optimization - guidance systems
Low thrust trajectory analysis - guidance systems
Trajectory requirements for terminal lunar landing from analog simulation of spacecraft
Trajectory simulation for stability and control studies of multiengine boosters
Guidance policies for multiple-impulse correction of spacecraft trajectory
Problems in computing transition matrices of lunar trajectories
Free flight circumlunar trajectories - motion analysis
Boost vehicle trajectories for ranger and mariner programs
Inversion of ordinary linear differential equation in matrix form for application to class of trajectory perturbation problems
Trajectory optimization technique based on theory of second variation
Optimal trajectory geometry and thrust programming
Nonlinear guidance system for descent trajectories
Determination of optimum 3-dimensional trajectories to inject a saturn c-5 rocket into a space-fixed circular orbit
Description and flight test results of the x-14a jet propelled vtol aircraft used to study lunar landing trajectories and control requirements
Inversion property of the fundamental matrix in trajectory perturbation problems