Add to ORKGThe potential effects of fly by wire and control configured vehicle concepts on flying qualities are considered. Failure mode probabilities and consequences, controllability, and dynamics of highly augmented aircraft are among the factors discussed in terms of design criteria
The development of more efficient control surfaces requiring less force to operate are presented
This thesis addresses the application issues raised implementing flight control designs derived from...
Vehicle design considerations for active control applications to subsonic transports are examined. A...
Flying quality requirements are specified in terms of the complete pilot-airframe-systems loop, the ...
The optimal control model for pilot vehicle systems was used to develop a methodology for predicting...
Fly-by-wire flight control systems are becoming more common in both civil and military aircraft. Th...
A summary of the YF-16 flight control system is presented. The basic functions of the flight control...
The introduction of fly-by-wire electronic flight control systems into transport aircraft has given...
Despite significant advancements in controls configured vehicles/active controls technology (CCV/ACT...
The advanced control technology is considered that is necessary to cope with the medium STOL transpo...
The flight control system design, though quite satisfactory on paper, many times gives surprises dur...
Aircraft designers are rapidly moving toward full fly by wire control systems for transport aircraft...
The state of the art in active control technology is summarized. How current design criteria and air...
The stability and control of a high-performance aircraft was analyzed, and a design methodology for ...
The notion of airplane stability and control being a balancing act between stability and control ha...
The development of more efficient control surfaces requiring less force to operate are presented
This thesis addresses the application issues raised implementing flight control designs derived from...
Vehicle design considerations for active control applications to subsonic transports are examined. A...
Flying quality requirements are specified in terms of the complete pilot-airframe-systems loop, the ...
The optimal control model for pilot vehicle systems was used to develop a methodology for predicting...
Fly-by-wire flight control systems are becoming more common in both civil and military aircraft. Th...
A summary of the YF-16 flight control system is presented. The basic functions of the flight control...
The introduction of fly-by-wire electronic flight control systems into transport aircraft has given...
Despite significant advancements in controls configured vehicles/active controls technology (CCV/ACT...
The advanced control technology is considered that is necessary to cope with the medium STOL transpo...
The flight control system design, though quite satisfactory on paper, many times gives surprises dur...
Aircraft designers are rapidly moving toward full fly by wire control systems for transport aircraft...
The state of the art in active control technology is summarized. How current design criteria and air...
The stability and control of a high-performance aircraft was analyzed, and a design methodology for ...
The notion of airplane stability and control being a balancing act between stability and control ha...
The development of more efficient control surfaces requiring less force to operate are presented
This thesis addresses the application issues raised implementing flight control designs derived from...
Vehicle design considerations for active control applications to subsonic transports are examined. A...