Choosing trajectory parameters to maximize mission of probability of success.
Mission success probability maximization by selecting trajectory parameters via approximate probability density function
TRAJECTORY OPTIMIZATION↗
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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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Three models of preview control.
Three models of constrained preview control with successive target values of nonuniform importance
DYNAMIC PROGRAMMING↗
Choosing trajectory parameters to maximize mission probability of success.
Mission success probability maximization by selecting trajectory parameters via approximate probability density function
MISSION PLANNING↗
Orbit determination with the Davidon method.
Orbit determination with Davidon method in obtaining maximum likelihood values
TRAJECTORY OPTIMIZATION↗
Jupiter swingby missions to the outer planets.
Jupiter swingby missions to outer planets
PLANETARY SPACE FLIGHT↗
A Method for Determining Optimum Re-entry Trajectories
Determining optimum atmospheric reentry trajectories using Pontryagin maximum principle
PONTRYAGIN PRINCIPLE↗
The utilization of an impulsive solution in solving optimum trajectory problems with bounded thrust magnitude
Impulsive solution used to solve optimum trajectory problems with bounded thrust magnitude
TRAJECTORY OPTIMIZATION↗
Spherical focused blast device
Focusing blast accuracy for antiaircraft missile warheads using a sphere of Composition C-4
ANTIAIRCRAFT MISSILE↗
The primer vector on fixed-time impulsive trajectories.
Primer vector of fixed-time impulsive thrust trajectories
TRAJECTORY OPTIMIZATION↗
Optimum deorbit positioning for minimum impulse reentry.
Optimum deorbit positioning on planetocentric elliptic orbit for single impulse reentry treated by two coupled quartic polynomials
ELLIPTICAL ORBIT↗
Quasilinearization determination of optimum finite-thrust orbital transfers.
Quasi-linearization determination of optimum finite thrust and impulsive orbital transfers
TRAJECTORY OPTIMIZATION↗
Optimum deorbit positioning for minimum impulse reentry.
Optimum deorbit positioning on planetocentric elliptic orbit for single impulse reentry treated by two coupled quartic polynomials
REENTRY PHYSICS↗
Rapid determination of near-optimum linear pitch programs for rocket boosters.
Linear segment pitch rate program for near optimum trajectory for rocket boosters
COMPUTER PROGRAM↗
Some Analytical Characteristics of the Optimum Two-Impulse Orbital Transfer Under Arbitrary Terminal Conditions
Optimum two-impulse orbital transfer for arbitrary terminal conditions, discussing analytic characteristics
TRAJECTORY OPTIMIZATION↗
Iterative guidance applied to generalized missions.
Iterative guidance mode /IGM/ applied to effective gravity vector prediction, acceleration measurement of noise sensitivity and energy limitations
ITERATIVE SOLUTION↗
Time-optimal rendezvous for elliptic orbits
Time optimal rendezvous trajectories for variable thrust intercepting and orbiting space vehicles
Alfriend, K. T.↗
Secondary mission optimization.
Secondary or abort mission maximized subject to primary mission constraints by variational treatment of optimal branched trajectories
Dickerson, W. D.↗
Effect of trajectory, guidance, and environmental parameters and uncertainties on the design optimization of a planetary landing vehicle.
Planetary landing vehicle design optimization, considering effects of trajectory, guidance and environmental parameters under uncertainty
Mukhopadhyay, A. K.↗