An Analytical Solution to Patched Conic Trajectories Satisfying Initial and Final Boundary Conditions
Analytical solution to patched conic trajectories satisfying initial and final boundary conditions
Carlson, K. M.↗
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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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Comparison of trajectory profiles and nuclear-propulsion-module arrangements for manned Mars and Mars-Venus missions
Trajectory profiles and nuclear propulsion vehicle configurations for manned Mars and Mars-Venus missions
Willis, E. A., Jr.↗
Singular perturbations and minimum fuel space trajectories
Perturbation theory for fuel space trajectory optimization
Edelbaum, T. N.↗
Control of a spinning drag-free satellite to reduce trajectory errors due to mass attraction
Control analysis of spinning drag free satellite controller to reduce trajectory errors from mass attraction
Jhin, P.↗
Real-gas effects on the drag and trajectories of a nonlifting 140 deg conical aeroshell during Mars entry
Real gas effects on drag and trajectories of nonlifting conical shell during Mars atmospheric entry
Allison, D. O.↗
Application of empirical Bayes decision procedures to discrete time linear filtering. Investigation of an empirical Bayes filter for use in trajectory estimation Final report
Empirical Bayes filter for use in trajectory estimation and comparison of performance with Kalman filter
Kamat, S. J.↗
Trajectory observations for some spiraling electron beam systems
Trajectory observations for some spiraling electron beam systems using moveable probes and targets as well as photographic techniques
Wilmarth, R. W.↗
Exponential downweighting of past data in a single stage, weighted-least-squares trajectory processor
Exponential downweighting of past data in single stage, weighted least squares trajectory processor for coasting spacecraft
Rich, R. G.↗
Design and implementation of models for the double precision trajectory program /DPTRAJ/
Development and numerical integration of differential equations of spacecraft motion used in Double Precision Trajectory Program
Spier, G. W.↗
Generalized multistep method as applied to trajectory determination
Multistep integration formula for orbit trajectory determination
Velez, C. E.↗
Performance verification trajectories for the McDonnell-Douglas high cross-range shuttle configuration
Space shuttle trajectory performance data for east and west test range launch simulations
Etheridge, O. E.↗
Orbiter entry trajectory control. 1 - High speed entry phase
Drag control method for space shuttle orbiter entry trajectory guidance
Mc Namara, J.↗
Orbiter entry trajectory control. 2 - Terminal phase entry
Terminal entry trajectory analysis for spiral glide descent of space shuttle to landing site
Weiss, L.↗
Minimum shuttle thermal protection system weight through trajectory shaping
Entry trajectory control effects on thermal protection system weight of space shuttle
Kipp, H. W.↗
Approximate trajectory data for missions to the major planets
Contour charts and tables on trajectory data for missions to Jupiter, Saturn, Uranus, and Neptune and their moons
Fishbach, L. H.↗
Thrusting trajectory minimization program for orbital transfer maneuvers
Computer program for transfer orbit trajectory optimization based on Lagrange multipliers, Newton-Raphson method, and power series
Green, R. N.↗
Midcourse and approach guidance requirements for simplified onboard control of moon to earth trajectories
Development of procedures for midcourse and approach guidance of moon to earth trajectories based on optical angular measurements and onboard calculations
Hamer, H. A.↗
Chebychev trajectory optimization program /CHEBYTOP 2/ Final report
Computer program for electric propelled spacecraft interplanetary, flyby, and rendezvous trajectory optimization based on Chebyshev approximation and polynomial representations
Hahn, D. W.↗