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Flight Path Control
Instrument Landing System Approaches
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20 Degree Spoiler aerodynamic center Aircraft Response airspeed Altitude Change feet altitude loss Analog Computer angle of attack Approach Task Approach with Bang-Bang Bang-Bang Position Spoilers Bang-Bang Rate Spoiler Beechcraft Duke coefficient Airplane control inputs control lift Conventional ILS Approach deg or rad Degree Spoiler Step descent rate control direct lift control evaluation pilots flight path control Flight Research Laboratory flight simulator ft/sec glide slope glideslope handling qualities Instrument Landing System l0 Second Spoiler landing approach lift coefficient light aircraft Load Factor modified Cardinal phugoid excitation phugoid motion Pilot A Mx Pilot G Pilot Performance Pitch Angle degrees Rate Spoiler Control Response to 20 RMS error Second Spoiler Pulse shown in Figure sp sp spdlc speed and pitch Speed Variation feet/second speedbrake Spoiler Deflection degrees spoiler drag spoiler inputs spoiler pitching spoiler position spoiler system Stability Derivatives switch trim speed University of Kansas Vertical Speed feet/minute visual approaches wheel