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 with no coupling. thereby simplifying the required co... https://www.chiggate.com/shades-eq-gloss-07m-driftwood-for-sale/