The state of the art of active controls technology (ACT) and a recommended ACT development program plan are reviewed. The performance benefits and cost of ownership of an integrated application of ACT to civil transport aircraft is to be assessed along with the risk and laboratory and/or flight experiments designed to reduce the technical risks to a commercially acceptable level.
Integrated Application of Active Controls (IAAC) Technology to an Advanced Subsonic Transport: Project Plan
1981
43 pages
Report
Keine Angabe
Englisch
Aircraft , Avionics , Aerodynamics , Active control , Control configured vehicles , Energy conservation , Subsonic aircraft , Transport aircraft , Transportation energy , Aeronautical engineering , Angle of attack , Self adaptive control systems , Stability augmentation , Technology utilization , Turbulence effects , Wing loading