Most UAV configurations are conventional, aerodynamically driven shapes, with conventional stability AND control characteristics. However, the requirements of Combat UAVs (UCAVs) drive to radical configurations with unusual stability AND control challenges: Finless - Rudderless - High wing sweep - Unusual wing shapes - Blended wing-bodies - No forebody. Stability AND control issues must be addressed early in the UCAV design cycle.
Stability & Control Aspects of UCAV Configurations
2002
19 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aircraft , Meetings , Control systems , Aerodynamic stability , Configurations , Drones , Maneuverability , Roll , Payload , Pitch(Inclination) , Yaw , Survivability , Swept wings , Long range(Distance) , Balance , Subsonic characteristics , Thrust vector control systems , Instability , Workshops , Split flaps , Medium altitude , Ucav(Unmanned combat air vehicle) , Briefing charts
Aeroacoustic Assessment of Low-Observable UCAV Configurations
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