A Flight Investigation of Systems Developed for Reducing Pilot Workload and Improving Tracking Accuracy During Noise-abatement Landing Approaches, Volume 1427
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AIRPLANE Airplane airplane attitude airplane center airport airspeed error ALTITUDE CONTROL 367-80 Altitude Control 367-80)-Pitch ALTITUDE CONTROL LTA Altitude Control LTA)-Pitch analog computer Autothrottle auxiliary flap axis flight director basic airplane C.G.-Basic Airplane center of gravity closed-loop command control inputs Control LTA)-Pitch Loop damping ratio dead zone deg/sec direct-lift control DLC modes downspring EADI evaluation pilot's FIGURE flight control flight director FLIGHT SAFETY FOUNDATION ft/sec glide slope grooved runways handling qualities high beam improvement inner loop Kh S2 landing flare Locus of Altitude Locus of Pitch longitudinal LOOP CLOSED Loop Closed-Pilot's Loop Open-Airplane Loop Open-Pilot's LTA configuration NASA Number operation Phase pilot workload pilot's station Pitch Attitude Control pitch attitude loop pitch axis pitch control pitch flight PITCH LOOP pitch rate rate command/attitude hold Root Locus runway grooving safety pilot shown in figs signal spoiler Station-Basic Airplane Station-DLC throttle touchdown two-beam approach