Requirements and possible solutions for control configured vehicles (CCV) are discussed. A review is given of control technology problems associated with CCV design, and research is reported on two specimen aircraft with regard to artificial stabilization. Requirements for maneuverability and dynamic behavior in longitudinal motion were established. A design for a damper-stabilizer system in an aircraft with an elastic elevator system was investigated for different suboptimal control unit structures with limited recovery capacity.
Control Configured Vehicles (Ccv)
1975
128 pages
Report
Keine Angabe
Englisch
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