NASA's current and projected advanced control technology programs for future transport aircraft include the design and verification of full flight envelope autopilots, the development and flight test of all-digital fly by wire systems, the evolution of low cost innovative avionics concepts such as split surface stability augmentation systems, the evaluation of integrated propulsion control and cooperative autopilot/propulsion control systems, the application of active control systems to short haul and long haul transports, and the demonstration of reconfigured active control aircraft. Key technical features and anticipated contributions of these technologies are outlined
NASA Dryden has been engaging in some exciting work that will enable lighter weight and more fuel ef...
A NASA program to develop digital fly-by-wire (DFBW) technology for aircraft applications is discuss...
Military aircraft research opportunities for the future are briefly surveyed. Aircraft control theor...
Aerodynamic and active control concepts for application to commercial transport aircraft are discuss...
Active controls improve airplane performance by stabilizing its flight, reducing departures from sta...
A summary is presented of results obtained during analysis, design and test activities on six select...
The feasibility of using digital fly-by-wire systems to control aircraft was demonstrated by develop...
At the NASA Armstrong Flight Research Center research is being conducted into flight control technol...
To assess the feasibility of a digital fly by wire system, the mechanical flight control system of a...
The topics covered include fly by wire, digital control, control configured vehicles, applications t...
The workshop consisted of 24 technical presentations on various aspects of aircraft controls, rangin...
The results of studies which were undertaken to contribute to the design of digital flight control s...
The application of active controls technology to subsonic, long-range transport aircraft was investi...
A flight research program was conducted to assess the improvements, in longitudinal path control dur...
In aerodynamics, the use of new and flexible tools for the design of supercritical wings is discusse...
NASA Dryden has been engaging in some exciting work that will enable lighter weight and more fuel ef...
A NASA program to develop digital fly-by-wire (DFBW) technology for aircraft applications is discuss...
Military aircraft research opportunities for the future are briefly surveyed. Aircraft control theor...
Aerodynamic and active control concepts for application to commercial transport aircraft are discuss...
Active controls improve airplane performance by stabilizing its flight, reducing departures from sta...
A summary is presented of results obtained during analysis, design and test activities on six select...
The feasibility of using digital fly-by-wire systems to control aircraft was demonstrated by develop...
At the NASA Armstrong Flight Research Center research is being conducted into flight control technol...
To assess the feasibility of a digital fly by wire system, the mechanical flight control system of a...
The topics covered include fly by wire, digital control, control configured vehicles, applications t...
The workshop consisted of 24 technical presentations on various aspects of aircraft controls, rangin...
The results of studies which were undertaken to contribute to the design of digital flight control s...
The application of active controls technology to subsonic, long-range transport aircraft was investi...
A flight research program was conducted to assess the improvements, in longitudinal path control dur...
In aerodynamics, the use of new and flexible tools for the design of supercritical wings is discusse...
NASA Dryden has been engaging in some exciting work that will enable lighter weight and more fuel ef...
A NASA program to develop digital fly-by-wire (DFBW) technology for aircraft applications is discuss...
Military aircraft research opportunities for the future are briefly surveyed. Aircraft control theor...