Low thrust interplanetary trajectory open loop error analysis, volume 1 Final report
Computer program for open-loop error analysis of low thrust interplanetary trajectories
Jazwinski, A. H.↗
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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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SWINGBY - A low thrust interplanetary swingby trajectory optimization program, volume 2 Final report
Segmented two-body low thrust interplanetary swingby trajectory and performance optimization program
Hipkins, C.↗
TRIP trajectory integration program
Computer program with predictor-corrector numerical integration subroutine for fast trajectory analysis
Kaufman, B.↗
Optimal round trip space tug trajectories for earth escape missions
Optimal round trip space tug trajectories for earth escape missions
Teren, F.↗
An examination of the effects of station longitude errors on Doppler plus range and Doppler only orbit determination solutions with an emphasis on a Viking mission trajectory
Station longitude error effects on Doppler plus range and Doppler only orbit determination solutions, emphasizing Viking mission trajectory
Ondrasik, V. J.↗
Molecular collisions. 16: Comparison of GPS with classical trajectory calculations of rotational inelasticity for the Ar-N2 system
Comparison of generalized phase shift treatment with classical trajectory calculations of rotational inelasticity cross sections of Ar-N2 scattering
Pattengill, M. D.↗
Trajectory and propulsion characteristics of comet rendezvous opportunities
Trajectory and propulsion characteristics of spacecraft rendezvous mission opportunities to comets during 1975 to 1995
Friedlander, A. L.↗
Approximate Optimal Atmospheric Entry Trajectories
Approximate optimal atmospheric entry trajectories maximizing terminal function of velocity, heading angle, flight path angle, and altitude
Speyer, J. L.↗
Preliminary determination of spacecraft trajectories using on-board optical measurements
Star selection and bias error eliminating calibrations for five onboard optical measurements used to determine spacecraft trajectories
Mclean, J. D.↗
Predictions on the characteristics of the minimal two-impulse orbital transfer under arbitrary terminal conditions by using the bounding trajectories
Predicting characteristics of minimal total impulse solution of two-terminal, two-impulse orbital transfer problem by using bounding trajectories
Sun, F. T.↗
Regularization and the computation of optimal trajectories
Continuous thrust spacecraft optimal trajectory regularization, obtaining differential equations for three dimensional motion
Tapley, B. D.↗
Postflight analysis including six-degree-of- freedom trajectory simulation of the behavior of an Aerobee 350 sounding rocket in the presence of a very large thrust misalignment
Postflight analysis including six degree of freedom trajectory digital simulation of Aerobee 350 sounding rocket behavior under large thrust misalignment
Lane, J. H.↗
The optimization of trajectories of linear functional differential equations
Linear functional differential equations trajectory optimization, proving maximal principle
Banks, H. T.↗
A study on the optimal rocket trajectory
Optimal vacuum rocket trajectories over spherical earth, deriving nonlinear differential equations for position and velocity
Burns, R. E.↗
Application of an impulsive trajectory optimization method to the comet rendezvous problem
Multiple impulsive spacecraft trajectory optimization technique application to comet rendezvous problem, using computer program
Waters, J. I.↗
An explicit midcourse guidance technique for lunar and interplanetary trajectories based upon matched asymptotic expansions
Spacecraft midcourse guidance technique for lunar and interplanetary trajectories based on matched asymptotic expansions
Carlson, N. A.↗
Mars lander deorbit trajectory analysis
Mars lander deorbit trajectory sensitivity analysis for fixed flight path and communications angles at atmospheric entry, comparing with Monte Carlo simulation
Euler, E. A.↗
Coordinate system influence on the regularized trajectory optimization problem
Numerical integration for continuously thrusting spacecraft optimal trajectory, considering rectangular Cartesian and polar cylindrical coordinates characteristics
Lewallen, J. M.↗