Despite significant advancements in controls configured vehicles/active controls technology (CCV/ACT) in the past decade, few applications of this promising technology have appeared in recent aircraft designs. The status of CCV/ACT is summarized, and some of the constraints which are retarding its wider application are described. Suggestions toward establishing an increased level of confidence in the technology are given
To assess the feasibility of a digital fly by wire system, the mechanical flight control system of a...
The implication of the dependence on active controls technology during the design phase of transport...
Flying quality requirements are specified in terms of the complete pilot-airframe-systems loop, the ...
The application of active controls technology to subsonic, long-range transport aircraft was investi...
Recently completed B-52 Control Configured Vehicles (CCV) flight testing is summarized, and results ...
The performance and economic benefits of a constrained application of Active Controls Technology (AC...
The development of an advanced, computerized method for the analysis and evaluation of the aeroelast...
The state of the art in active control technology is summarized. How current design criteria and air...
An active controls technology (ACT) system architecture was selected based on current technology sys...
The potential effects of fly by wire and control configured vehicle concepts on flying qualities are...
A set of digital flight control laws were designed for the NASA F-8C digital fly-by-wire aircraft. T...
NASA's current and projected advanced control technology programs for future transport aircraft incl...
A summary of the YF-16 flight control system is presented. The basic functions of the flight control...
Active controls improve airplane performance by stabilizing its flight, reducing departures from sta...
Vehicle design considerations for active control applications to subsonic transports are examined. A...
To assess the feasibility of a digital fly by wire system, the mechanical flight control system of a...
The implication of the dependence on active controls technology during the design phase of transport...
Flying quality requirements are specified in terms of the complete pilot-airframe-systems loop, the ...
The application of active controls technology to subsonic, long-range transport aircraft was investi...
Recently completed B-52 Control Configured Vehicles (CCV) flight testing is summarized, and results ...
The performance and economic benefits of a constrained application of Active Controls Technology (AC...
The development of an advanced, computerized method for the analysis and evaluation of the aeroelast...
The state of the art in active control technology is summarized. How current design criteria and air...
An active controls technology (ACT) system architecture was selected based on current technology sys...
The potential effects of fly by wire and control configured vehicle concepts on flying qualities are...
A set of digital flight control laws were designed for the NASA F-8C digital fly-by-wire aircraft. T...
NASA's current and projected advanced control technology programs for future transport aircraft incl...
A summary of the YF-16 flight control system is presented. The basic functions of the flight control...
Active controls improve airplane performance by stabilizing its flight, reducing departures from sta...
Vehicle design considerations for active control applications to subsonic transports are examined. A...
To assess the feasibility of a digital fly by wire system, the mechanical flight control system of a...
The implication of the dependence on active controls technology during the design phase of transport...
Flying quality requirements are specified in terms of the complete pilot-airframe-systems loop, the ...