Add to ORKGThis study focuses on use of the Transport Systems Research Vehicle (TSRV) Simulator at the Langley Research Center to obtain pilot opinion and input on the Federal Aviation Administration's Runway Status Light System (RWSL) prior to installation in an operational airport environment. The RWSL has been designed to reduce the likelihood of runway incursions by visually alerting pilots when a runway is occupied. Demonstrations of the RWSL in the TSRV Simulator allowed pilots to evaluate the system in a realistic cockpit environment
The Hazardous and Solid Waste Amendment portion of the National Aeronautics and Space Administration...
The role of flight instrumentation and control systems in the advancement of civil aviation to the s...
The Real-Time Failure Control (RTFC) program involves development of a failure detection algorithm, ...
The U.S. Air Force Remotely Piloted Aircraft and Unmanned Aerial Vehicle Strategic Vision (hereafter...
Pilots' use of and responses to a traffic alert and collision-avoidance system (TCAS 2) in simulated...
A Linear Quadratic Regulator synthesis technique was used to design an explicit model following cont...
The space operations incident reporting tool (SOIRT) is an instrument used to record information abo...
This document presents the solar electric propulsion (SEP) concept design developed as part of the S...
A propulsion-controlled aircraft (PCA) system for emergency flight control of aircraft with no fligh...
An investigation of the wing upper surface flow-field disturbance due to in-flight inboard thrust re...
A ROTO architecture, braking and steering control law and display designs for a research high speed ...
The Terminal Configured Vehicle (TCV) program operates a Boeing 737 modified to include a second coc...
The NASA Dryden Flight Research Center has flight tested two X-29A aircraft at low and high angles o...
The National Aeronautics and Space Administration (NASA) Commercial Crew Program (CCP) has been char...
Functional shock, safety, overall system costs, and emergence of new technologies, have raised conce...
The Hazardous and Solid Waste Amendment portion of the National Aeronautics and Space Administration...
The role of flight instrumentation and control systems in the advancement of civil aviation to the s...
The Real-Time Failure Control (RTFC) program involves development of a failure detection algorithm, ...
The U.S. Air Force Remotely Piloted Aircraft and Unmanned Aerial Vehicle Strategic Vision (hereafter...
Pilots' use of and responses to a traffic alert and collision-avoidance system (TCAS 2) in simulated...
A Linear Quadratic Regulator synthesis technique was used to design an explicit model following cont...
The space operations incident reporting tool (SOIRT) is an instrument used to record information abo...
This document presents the solar electric propulsion (SEP) concept design developed as part of the S...
A propulsion-controlled aircraft (PCA) system for emergency flight control of aircraft with no fligh...
An investigation of the wing upper surface flow-field disturbance due to in-flight inboard thrust re...
A ROTO architecture, braking and steering control law and display designs for a research high speed ...
The Terminal Configured Vehicle (TCV) program operates a Boeing 737 modified to include a second coc...
The NASA Dryden Flight Research Center has flight tested two X-29A aircraft at low and high angles o...
The National Aeronautics and Space Administration (NASA) Commercial Crew Program (CCP) has been char...
Functional shock, safety, overall system costs, and emergence of new technologies, have raised conce...
The Hazardous and Solid Waste Amendment portion of the National Aeronautics and Space Administration...
The role of flight instrumentation and control systems in the advancement of civil aviation to the s...
The Real-Time Failure Control (RTFC) program involves development of a failure detection algorithm, ...