367-80 airplane variable stability simulation system /NASA Langley supersonic transport simulation program/
Four-engine jet aircraft used as in-flight simulator for variable stability testing of supersonic aircraft
JET AIRCRAFT↗
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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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Simulation of three supersonic transport configurations with the Boeing 367-80 in-flight dynamic simulation airplane
In-flight dynamic simulator used to evaluate problems of low-speed approach and landing of supersonic transport
LOW SPEED STABILITY↗
367-80 variable stability simulation system /NASA Ames large transport simulation program/
Boeing 707 aircraft for in-flight dynamic approach and landing simulation of large subsonic transport aircrafts
SUBSONIC SPEED↗
Space thermal simulation, without a solar simulator.
Thermal energy balance of orbiting spacecraft simulated, using tungsten-filament lamp without duplicating solar spectrum
THERMAL PROTECTION↗
Simulation and experimental-techniques. Part I - Simulation of liquid sloshing
Dimensional analysis applied to simulation of liquid sloshing
LIQUID SLOSHING↗
A Study of the Navigator's Sighting Accuracy Using a Simulated Vehicle-Mounted Space Sextant and a Description of the Sextant Simulator
Sextant simulator for midcourse guidance of manned spacecraft during interstellar travel
MIDCOURSE GUIDANCE↗
Plane-flame simulation of the wake behind an internally propelled vehicle. Part 3 - Experimental simulation of a supersonic vehicle by a detonation
Detonation wave simulation of flow field induced by supersonic vehicle
Skinner, J. H., Jr.↗
Digital autopilot simulation for the LM mission simulator.
Real time interpretive simulation of lunar module digital autopilot program for flight crew training
Croston, R. C.↗
Planetary environment simulation - Martian sand and dust storm simulation and evaluation, volume 2
Particle behavior in simulated Martian sand and dust storm
Adlon, G. L.↗
Apollo simulation and simulators - A demand bibliography
Bibliography of flight simulation for Apollo project
Source record↗
An airborne simulator program to determine if roll-mode simulation should be a moving experience
Airborne simulator program for evaluation of motion and visual cue effects on pilot performance in roll, using compensatory tracking tasks
Deets, D. A.↗
Simulation and simulator development of a separate surface attitude command control system for light aircraft
A detailed description is presented of the simulation philosophy and process used in the development of a Separate Surface Attitude Command control system (SSAC) for a Beech Model 99 Airliner. The intent of this system is to provide complete three axes stability augmentation at low cost and without the need for system redundancy. The system, although aimed at the general aviation market, also has applications to certain military airplanes as well as to miniature submarines.
Roskam, J.↗
Simulation verification techniques study. Task report 4: Simulation module performance parameters and performance standards
Shuttle simulation software modules in the environment, crew station, vehicle configuration and vehicle dynamics categories are discussed. For each software module covered, a description of the module functions and operational modes, its interfaces with other modules, its stored data, inputs, performance parameters and critical performance parameters is given. Reference data sources which provide standards of performance are identified for each module. Performance verification methods are also discussed briefly.
Source record↗
A technique for simulating turbulence for aerospace vehicle flight simulation studies
An atmospheric turbulence model which accommodates variability of turbulence properties along an aerospace vehicle trajectory was developed. The technique involves the use of Dryden spectral forms in which the defining parameters are the standard deviations (sigma) and integral scales (L) of turbulence. These spectra are expressed as nondimensional functions of the nondimensional frequency Omega = omega L/V where omega is dimensional radian frequency and V is the true air speed of the aerospace vehicle. The nondimensional spectra are factored by standard techniques to obtain nondimensional linear recursive filters in the time domain whereby band-limited white-like noise can be operated upon to obtain nondimensional longitudinal, lateral, and vertical turbulence velocities, as functions of nondimensional time, tV/L, where t is time. Application of the technique to the simulation of the space shuttle orbiter entry flight phase is discussed.
Fichtl, G. H.↗
Standalone engine simulator (SAES), Engine Dynamics simulator (EDS) Xerox Sigma 5 interface hardware manual
The ESS-EDS and EDS-Sigma interfaces within the standalone engine simulator are described. The operation of these interfaces, including the definition and use of special function signals and data flow paths within them during data transfers, is presented along with detailed schematics and circuit layouts of the described equipment.
Kirshten, P. M.↗
The analysis of delays in simulator digital computing systems. Volume 1: Formulation of an analysis approach using a central example simulator model
The effects of spurious delays in real time digital computing systems are examined. Various sources of spurious delays are defined and analyzed using an extant simulator system as an example. A specific analysis procedure is set forth and four cases are viewed in terms of their time and frequency domain characteristics. Numerical solutions are obtained for three single rate one- and two-computer examples, and the analysis problem is formulated for a two-rate, two-computer example.
Heffley, R. K.↗
Solar Power Satellite antenna phase control system hardware simulation, phase 4. Volume 2: Analytical simulation of SPS system performance
The pilot signal parameter optimization and power transponder analyses are presented. The SPS antenna phase control system is modeled and the hardware simulation study described. Ionospheric and system phase error effects and the effects of high power amplifier phase and amplitude jitters are considered. Parameter optimization of the spread spectrum receiver, consisting of the carrier tracking loop and the code tracking loop, is described.
Lindsey, W. C.↗
Network simulation using the simulation language for alternate modeling (SLAM 2)
The simulation language for alternate modeling (SLAM 2) is a general purpose language that combines network, discrete event, and continuous modeling capabilities in a single language system. The efficacy of the system's network modeling is examined and discussed. Examples are given of the symbolism that is used, and an example problem and model are derived. The results are discussed in terms of the ease of programming, special features, and system limitations. The system offers many features which allow rapid model development and provides an informative standardized output. The system also has limitations which may cause undetected errors and misleading reports unless the user is aware of these programming characteristics.
Shen, S.↗