Teleprocessing system 7740-7010 workload analysis Final report
Computer simulation model for overload prediction in teleprocessing system with additional terminals, and workloads
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.
Computer simulation model for overload prediction in teleprocessing system with additional terminals, and workloads
Analog computer simulation to assess random sampling interval effects on sampled data model of human operator
Equations and logic for digital computer simulation of environmental pressure effects on earth-orbiting satellites
Requirements specification and analysis of dynamic simulation methods for launch vehicle component level simulation computer program
Hydrodynamical and mechanical design layout for two-speed hydraulic turbine inducer, computer simulation of pumping system and test facility performance, and study of demonstration unit
Computer simulation studies of codes applicable to deep space telemetry links
Recursive techniques for digital signal processing, data smoothing and compression, and computer simulation of low error rate communication
Computer simulation investigation of control and tracking problems associated with optical communication systems for deep space probes
Equations for active control system of generalized spacecraft simulation computer program
Gravity gradient satellite stabilization and performance analyzed, using computer simulation of motion equations, including eddy current dampers, solar effect, orbital eccentricity, etc
Computer simulated physical characteristics of electrically propelled spacecraft for selecting and designing attitude control system
This Phase II Body-Fixed, Three-Axis Reference System Study Final Report is the result of a follow-on contract awarded by NASAIMSFC to TRW Systems in April 1966, under Contract No, NASS-20209. of the Phase I1 Study was to refine and supplement the strapdown inertial ’ reference assembly (SIRA), software, airborne computer, and alignment analyses performed during Phase I of the same contract. The purpose Specifically, the Phase I results in many areas were those which could be achieved using simplifying assumptions (linearization) and hand analyses. It was the purpose of the Phase I1 studies to investigate the validity of the Phase I results by means of more sophisticated computer simulations, in which no simplifying assumptions were made, for each of the areas analyzed. The Phase 11 analyses were directed, therefore, at confirming the analytical feasibility asserted by the Phase I results.
Computer simulation and noise measurements of reentrant stream crossed-field amplifiers
Similarities between experimentally measured power spectral density curves of landing radar signal returned from rough surface and computer simulated curves for sinusoidal surfaces
Computer simulation of six degree of freedom flight equations
Digital signal processing, data smoothing, and computer simulation
Specifications for automatic storage and playback /ASAP/ and Saturn simulation computer program, and predicted data tape program
Feasibility study of hydromechanical actuator using analog computer simulation