Interplanetary Guidance System Requirements Study. Volume 2 - Computer Program Description. Part 3 - Nominal Powered Flight Trajectories
Computer programs for simulating booster nominal trajectories for interplanetary missions
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Computer programs for simulating booster nominal trajectories for interplanetary missions
Computer program for simulating lifting vehicle atmospheric entry flight trajectory
Computer program for simulating single-pass and single-skipout trajectories for lifting reentry vehicles
Double precision digital computer program for computing parameters and initial conditions of matched heliocentric and planetocentric phases of interplanetary trajectories
Computer program for optimization of low thrust interplanetary trajectories assuming constant and continuous thrust from given initial and final position, velocity and flight time
Analytical formulations and numerical integration methods for many body problem and special perturbative techniques
Coordinate measuring system for flight control, and trajectory optimization
Differential equations for governing motion of vehicle in uniform gravitational fields
Three numerical procedures for Mayer classical and non-classical problems in trajectory optimization
Observation theory and sensors applicable to navigation of boost and space vehicles
Maxima-minima theory, Pontryagin principle, and calculus of variations for optimal trajectory and control analysis
Mission constraints and trajectory interfaces for launch, rendezvous, spatial, deorbit, and entry phases of earth orbital mission
Simulator study of pilot control over lunar module during ascent from lunar surface
Pioneer 6 space probe spin stabilized orientation control system design survey
Automation of variational methods for solution of optimum control problems, optical data sources for Mars-encounter earth-based orbit determination, and operational support equipment
Trajectory synthesis for variable point mass, constant thrust, fixed staging time vehicles in vacuum
Quasi-optimum steering law for minimum time orbital injection rocket booster
Galactic Jupiter probe missions to make interstellar space measurements using Jupiter gravity assisted trajectories, discussing earth- Jupiter transfer orbits and mission parameters