A descent algorithm for constrained stochastic extrema.
Descent algorithm for finding stochastic extremum for situations not suited to optimal feedback control
SEARCH · Search NASA
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Descent algorithm for finding stochastic extremum for situations not suited to optimal feedback control
Lunar module descent engine exhaust effect on lunar surface temperatures
Radar-inertial navigator systems mechanization performance for terminal descent trajectory navigation of planetary lander
Trajectory optimization by descent process using hybrid computer for direct cost gradient computation
Zond-6 circumlunar flight and controlled descent landing in U.S.S.R.
Optimizing spacecraft televisions for successive picture overlapping and maximum surface resolution during planetary descent
Requirement estimates and performance predictions for Martian television experiment onboard spacecraft in three point-mass descent trajectories
Computer program for optimization of two-impulse transfers by contouring and steep descent
Automatic stations descent in planetary atmospheres as means of measurement data control
Simulation program for parachute and terminal descent phases of Mars soft lander
Hybrid conjugate gradient-steepest descent algorithms for unconstrained minimization
Apollo 10 descent propulsion system performance
Minimum fuel attitude control of spacecraft by Pontryagin principle and extended steepest descent method
Space vehicle trajectory optimization using computerized step by step steepest descent to minimum cost, considering cost gradient vs control
Ground based guidance for land-landing manned spacecraft with low velocity descent systems, discussing high and low altitude glide path intercept and spiral
Improved liner for Apollo lunar module descent engine injection chamber
Summary of material and design improvements to reduce ablative chamber throat erosion in lunar module descent engine
Atmospheric and near planet trajectory optimization by steepest descent method