Monte Carlo simulation of an adaptive policy for multiple impulse correction of the trajectory of a spacecraft.
Monte Carlo simulation for adaptive policy for multiple impulse correction of trajectory of spacecraft
SEARCH · Engineering Papers
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.
Monte Carlo simulation for adaptive policy for multiple impulse correction of trajectory of spacecraft
Computer-aided optimization using Monte Carlo techniques for digital systems timing
Monte Carlo transport calculations estimating solar flare proton radiation dose received by travelers during supersonic flight
Monte Carlo type computer simulation, programmed in Algol, for modeling reliability growth
Monte Carlo analysis of sphere transmission data for gold and iodine slow neutron capture cross sections at 24 keV
Monte Carlo simulation for Apollo go, no-go verification
Monte Carlo code for solving planar electron- diode problems including electron-neutral elastic collisions
Gamma-ray isotropic dose, energy flux and energy current buildup factors for finite slabs calculated by Monte Carlo techniques
Monte Carlo computer analysis of free molecular flow characteristics of thermosphere probe
Light reflection and transmission from clouds with various drop size distributions calculated using Monte Carlo technique
Monte Carlo program for calculating Doppler coefficients in arbitrary neutron flux spectra
MORL system reliability analysis, discussing Monte Carlo simulation, major parameters, constraints, program contingencies, etc
Transmission probability describing free molecular flow through vacuum systems obtained via Monte Carlo program
Monte Carlo approach to transition and free molecular flow problems having mass as well as thermal motion of molecules
Minimum variance simulation for satellite attitude determination reliability using magnetic and solar measurements
Rocket engine cluster thrust and moment vectors analyzed statistically for thrust misalignment
Three dimensional unsteady and steady sediment distribution obtained by Monte Carlo simulation method, using stochastic hydrodynamics model for transport
Sequential processor performance prediction error with linear method from Monte Carlo cycle analysis of Apollo 14 early rendezvous profile