Trajectory optimization by a direct descent process
Trajectory optimization by direct descent to minimum cost using iterative computer solutions
Fogarty, L. E.↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Some recent results in aerospace vehicle trajectory optimization techniques
Algorithms and computation techniques for solving trajectory optimization problems
Bauman, E. J.↗
Influence of uncertainties in the astronomical unit conversion and Mars planetary mass on Earth-Mars trajectories
Influence of uncertainties in planetary mass of Mars and astronomical unit on Earth-Mars trajectories
Rohde, P. J.↗
Trajectory optimization using fast-time repetitive computation
Perturbation method of computing optimum trajectories on hybrid and digital computers
Raby, J. S.↗
A trajectory code for maximizing the payload of multistage launch vehicles
Computer program for trajectory optimization and payload maximization in multistage launch vehicles
Spurlock, O. F.↗
Parametric Angles of Trajectory Determined Field Line Intersects
Parametric angles of trajectory determined field line intersections for production of artificial auroras
Stassinopoulos, E. G.↗
Study of trajectories and upper stage propulsion requirements for exploration of the solar system. Volume 1 - Summary Final report
Computer programs for solving trajectory and system optimization problems of electrically propelled interplanetary spacecraft for solar system exploration
Ragsac, R. V.↗
Study of trajectories and upper stage propulsion requirements for exploration of the solar system. Volume 2 - Technical report Final report, Aug. 1966 - Sep. 1967
Optimizing propulsion systems and trajectories of interplanetary spacecraft - numerical analyses and computer programs
Ragsac, R. V.↗
A survey of impulsive trajectories Final report
Literature survey of astrodynamics problems on intercept, transfer, and rendezvous trajectories
Doll, J. R.↗
A semigraphical method for a deorbit trajectory design study
Semigraphical method to aid selection of descent trajectory compatible with mission constraints
Green, R. N.↗
Trajectory Analysis and Guidance Theory Second Compilation of Papers, 1 Oct. 1966 - 1 Oct. 1967
Spacecraft guidance, trajectory analysis, and celestial mechanics - conference
Source record↗
Variations of parameters for trajectory integrations by modern perturbation differentiation methods. I.
Parameter variations method for trajectory integrations using perturbation differentiation of integrals of two body problem
Herrick, S.↗
Primer vector on fixed-time impulsive trajectories.
Primer vector of fixed time impulsive thrust trajectories
Handelsman, M.↗
Interplanetary trajectory selection criteria for Voyager Mars missions.
Trajectory design criteria for Voyager Mars missions toward standardization of launch vehicle, shroud, spacecraft bus, capsule and propulsion systems
Stavro, W.↗
Extension of the finite-difference Newton- Raphson algorithm to the simultaneous optimization of trajectories and associated parameters.
Finite difference Newton-Raphson algorithm extension to solve variational equations for simultaneous optimization of trajectories and associated parameters
Van Dine, C. P.↗
On randomly perturbed spacecraft trajectories.
Statistics of spacecraft trajectories perturbed by random forces
Wesseling, P.↗
Optimal payload trajectory characteristics for horizontally launched booster vehicle.
Optimal payload lifting and nonlifting trajectories of winged boost-launch vehicle
Elliott, J. R.↗
A two-variable asymptotic solution for three- dimensional solar powered low-thrust trajectories in the vicinity of the ecliptic plane.
Approximate analytic solution for variables describing three dimensional solar powered heliocentric low thrust trajectory in vicinity of ecliptic plane
Wesseling, P.↗