Paramount to proper utilization of electronic displays is a method for determining pilot-centered display requirements. Display design should be viewed fundamentally as a guidance and control problem which has interactions with the designer's knowledge of human psychomotor activity. From this standpoint, reliable analytical models of human pilots as information processors and controllers can provide valuable insight into the display design process. A relatively straightforward, nearly algorithmic procedure for deriving model-based, pilot-centered display requirements was developed and is presented. The optimal or control theoretic pilot model serves as the backbone of the design methodology, which is specifically directed toward the synthes...
Television-type, out-window visual simulation image generator design and specifications for aircraft...
Satellite berthing mechanism, umbilicals for fluid and electrical interfaces, EVA service platform, ...
A two dimensional cascade of harmonically oscillating airfoils was designed to model a near tip sect...
A guidance, navigation, and control system, the Simulated Shuttle Flight Test System (SS-FTS), when ...
The navigation and flight director guidance systems implemented in the NASA/FAA helicopter microwave...
High rate multiplexes asymmetry and jitter, data-dependent amplitude variations, and transition dens...
The formulation and implementation of navigation systems used for research investigations in the V/S...
The feasibility of classifying an airport terminal area for multipath effects, i.e., fadeout potenti...
Problems of commuter airplane configuration design were studied to affect a minimization of direct o...
Six scientific objectives/experiments were derived which consisted of agriculture/forestry/range res...
An optimizing computer program determined the turboprop aircraft with lowest direct operating cost f...
The definition of standard flight segments of phases, representing flight profile components which c...
Requirements are presented for the ascent/descent (A/D) navigation and attitude-dependent ancillary ...
Effects of aircraft dynamic characteristics on passenger ride quality are investigated to determine ...
A previously developed experimental air revitalization system was tested cyclically and parametrical...
Television-type, out-window visual simulation image generator design and specifications for aircraft...
Satellite berthing mechanism, umbilicals for fluid and electrical interfaces, EVA service platform, ...
A two dimensional cascade of harmonically oscillating airfoils was designed to model a near tip sect...
A guidance, navigation, and control system, the Simulated Shuttle Flight Test System (SS-FTS), when ...
The navigation and flight director guidance systems implemented in the NASA/FAA helicopter microwave...
High rate multiplexes asymmetry and jitter, data-dependent amplitude variations, and transition dens...
The formulation and implementation of navigation systems used for research investigations in the V/S...
The feasibility of classifying an airport terminal area for multipath effects, i.e., fadeout potenti...
Problems of commuter airplane configuration design were studied to affect a minimization of direct o...
Six scientific objectives/experiments were derived which consisted of agriculture/forestry/range res...
An optimizing computer program determined the turboprop aircraft with lowest direct operating cost f...
The definition of standard flight segments of phases, representing flight profile components which c...
Requirements are presented for the ascent/descent (A/D) navigation and attitude-dependent ancillary ...
Effects of aircraft dynamic characteristics on passenger ride quality are investigated to determine ...
A previously developed experimental air revitalization system was tested cyclically and parametrical...
Television-type, out-window visual simulation image generator design and specifications for aircraft...
Satellite berthing mechanism, umbilicals for fluid and electrical interfaces, EVA service platform, ...
A two dimensional cascade of harmonically oscillating airfoils was designed to model a near tip sect...