A two part investigation was conducted to determine the display requirements for the final approach and landing phase of a remotely piloted vehicle (RPV) mission, and to assess the relative merits of several possible display configurations. The objective of the first part of the investigation was to obtain subjective assessments of several display configurations, and to select the most promising display concepts for subsequent evaluation in terms of performance measures. A basic display consisting of a perspective image of terrain and runway, a horizon bar and an aircraft symbol was used, and guidance symbology was added to the basic displaying selected state variables. Initial results suggested that as guidance symbology is added to the ba...
A piloted simulation experiment was conducted using the NASA Ames Research Center Vertical Motion Si...
In the presented study a status display for supervisory control of multiple Medium Altitude Long End...
An electronic flight-guidance display format was designed for use in evaluations of the collimated h...
A simulator evaluation of a remotely piloted research vehicle was conducted at NASA Ames Research Ce...
A study of the display requirements for final approach management of the space shuttle orbiter vehic...
A computer drawn instrument landing approach display, which shows a box located on the desired path,...
A flight program was conducted to develop a landing technique with which a pilot could consistently ...
Effect of several variations of two types of TV display visual simulation systems on subjective pilo...
The results of a flight evaluation of two electronic display formats for the approach to landing und...
A study of the display requirements for final approach management of the space shuttle orbiter vehic...
Two computer generated display formats were evaluated as primary displays by six research pilots in ...
A set of flight tests designed to evaluate the relative utility of candidate displays with advanced ...
A computerized analysis procedure, based on a control theoretic model of the human pilot, is used to...
The results of a piloted-simulation evaluation of the benefits of adding runway symbology and track ...
A flight director adaptable to general aviation aircraft was evaluated for the landing approach task...
A piloted simulation experiment was conducted using the NASA Ames Research Center Vertical Motion Si...
In the presented study a status display for supervisory control of multiple Medium Altitude Long End...
An electronic flight-guidance display format was designed for use in evaluations of the collimated h...
A simulator evaluation of a remotely piloted research vehicle was conducted at NASA Ames Research Ce...
A study of the display requirements for final approach management of the space shuttle orbiter vehic...
A computer drawn instrument landing approach display, which shows a box located on the desired path,...
A flight program was conducted to develop a landing technique with which a pilot could consistently ...
Effect of several variations of two types of TV display visual simulation systems on subjective pilo...
The results of a flight evaluation of two electronic display formats for the approach to landing und...
A study of the display requirements for final approach management of the space shuttle orbiter vehic...
Two computer generated display formats were evaluated as primary displays by six research pilots in ...
A set of flight tests designed to evaluate the relative utility of candidate displays with advanced ...
A computerized analysis procedure, based on a control theoretic model of the human pilot, is used to...
The results of a piloted-simulation evaluation of the benefits of adding runway symbology and track ...
A flight director adaptable to general aviation aircraft was evaluated for the landing approach task...
A piloted simulation experiment was conducted using the NASA Ames Research Center Vertical Motion Si...
In the presented study a status display for supervisory control of multiple Medium Altitude Long End...
An electronic flight-guidance display format was designed for use in evaluations of the collimated h...