ADVANCES IN ALL-SOLID-STATE PASSIVELY Q-SWITCHED LASERS BASED ON CR4+:YAG SATURABLE ABSORBER


Coordinated Roll Control of Conformal Finless Flying Wing Aircraft

Attitude control of tailless aircraft is typically achieved through a system of trailing-edge flaps that produce coupled control effects in pitch, roll and yaw due to changes in lift and drag distributions.This paper presents a novel control allocation method which allows conformal trailing-edge controls to generate yawing moments telemarkskongen f

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