The kinematic parameters of position, velocity, and acceleration of a flight simulator may be calculated by knowing the distance between two or more points on an axis and the time the simulator takes to traverse the space between each set of points. These parameters are calculated through the use of difference techniques. Given the true kinematic response of the simulator to computer generated commands, the entire motion system loop may be calibrated, and system operability verified
The paper describes a method for guiding a dynamic system through a given set of points. The paradig...
A turbulent air motion measurement system (TAMMS) was integrated onboard the Lockheed 188 Electra ai...
A flightworthy active control landing gear system for a supersonic aircraft was designed to minimize...
The effects on eye scan behavior of both simulator and aircraft motion and sensitivity of an oculome...
Helicopter handling qualities research requires that a ground-based simulation be a high-fidelity re...
The development, evaluation, and evaluation results of a DC-9-10 runway directional control simulato...
Landings by experienced airline pilots transitioning to the DC-10, performed in flight and on a simu...
A standard kinematic model for aircraft simulation exists at NASA-Ames on a variety of computer syst...
Development and evaluation of experimental test plan for solutions of motion drive problem in format...
Development and characteristics of simulation concept to analyze man, machine, and environment aspec...
The researchers at the Langley Research Center Flight Simulation Computing System are provided with ...
The simulation and evaluation of proposed path selection systems for an autonomous Martian roving ve...
Fast Fourier Transform (FFT) and Least Square Error (LSE) estimation techniques were applied to the ...
The various techniques that have been used in the field of vehicle simulation and that are likely to...
A six-degree-of-freedom simulation analysis has been performed for the Space Shuttle Orbiter during ...
The paper describes a method for guiding a dynamic system through a given set of points. The paradig...
A turbulent air motion measurement system (TAMMS) was integrated onboard the Lockheed 188 Electra ai...
A flightworthy active control landing gear system for a supersonic aircraft was designed to minimize...
The effects on eye scan behavior of both simulator and aircraft motion and sensitivity of an oculome...
Helicopter handling qualities research requires that a ground-based simulation be a high-fidelity re...
The development, evaluation, and evaluation results of a DC-9-10 runway directional control simulato...
Landings by experienced airline pilots transitioning to the DC-10, performed in flight and on a simu...
A standard kinematic model for aircraft simulation exists at NASA-Ames on a variety of computer syst...
Development and evaluation of experimental test plan for solutions of motion drive problem in format...
Development and characteristics of simulation concept to analyze man, machine, and environment aspec...
The researchers at the Langley Research Center Flight Simulation Computing System are provided with ...
The simulation and evaluation of proposed path selection systems for an autonomous Martian roving ve...
Fast Fourier Transform (FFT) and Least Square Error (LSE) estimation techniques were applied to the ...
The various techniques that have been used in the field of vehicle simulation and that are likely to...
A six-degree-of-freedom simulation analysis has been performed for the Space Shuttle Orbiter during ...
The paper describes a method for guiding a dynamic system through a given set of points. The paradig...
A turbulent air motion measurement system (TAMMS) was integrated onboard the Lockheed 188 Electra ai...
A flightworthy active control landing gear system for a supersonic aircraft was designed to minimize...