Add to ORKGVehicle design considerations for active control applications to subsonic transports are examined. Active control is defined along with those functions which are considered in the study of design criteria. The FAA regulations governing transport aircraft design are briefly discussed
The Wing Planform Study and Final Configuration Selection Task of the Integrated Application of Acti...
The Current and Advanced Technology ACT control system definition tasks of the Integrated Applicatio...
Active wing load alleviation to extend the wing span by 5.8 percent, giving a 3 percent reduction in...
The state of the art in active control technology is summarized. How current design criteria and air...
The application of active controls technology to subsonic, long-range transport aircraft was investi...
The performance and economic benefits of a constrained application of Active Controls Technology (AC...
An effort to develop techniques for the design of integrated, fully automatic flight control systems...
The ALDCS development and design tasks, ALDCS functional configuration, and resulting challenges enc...
The implication of the dependence on active controls technology during the design phase of transport...
The active control concepts which achieve the benefit of improved mission performance and lower cost...
The potential effects of fly by wire and control configured vehicle concepts on flying qualities are...
Despite significant advancements in controls configured vehicles/active controls technology (CCV/ACT...
The active control technology (ACT) control/guidance system task of the integrated application of ac...
A review of analytical methods and associated tools for active controls analysis and design problems...
An active controls technology (ACT) system architecture was selected based on current technology sys...
The Wing Planform Study and Final Configuration Selection Task of the Integrated Application of Acti...
The Current and Advanced Technology ACT control system definition tasks of the Integrated Applicatio...
Active wing load alleviation to extend the wing span by 5.8 percent, giving a 3 percent reduction in...
The state of the art in active control technology is summarized. How current design criteria and air...
The application of active controls technology to subsonic, long-range transport aircraft was investi...
The performance and economic benefits of a constrained application of Active Controls Technology (AC...
An effort to develop techniques for the design of integrated, fully automatic flight control systems...
The ALDCS development and design tasks, ALDCS functional configuration, and resulting challenges enc...
The implication of the dependence on active controls technology during the design phase of transport...
The active control concepts which achieve the benefit of improved mission performance and lower cost...
The potential effects of fly by wire and control configured vehicle concepts on flying qualities are...
Despite significant advancements in controls configured vehicles/active controls technology (CCV/ACT...
The active control technology (ACT) control/guidance system task of the integrated application of ac...
A review of analytical methods and associated tools for active controls analysis and design problems...
An active controls technology (ACT) system architecture was selected based on current technology sys...
The Wing Planform Study and Final Configuration Selection Task of the Integrated Application of Acti...
The Current and Advanced Technology ACT control system definition tasks of the Integrated Applicatio...
Active wing load alleviation to extend the wing span by 5.8 percent, giving a 3 percent reduction in...