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Flight Path Control
Instrument Landing System Approaches
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20 Degree Spoiler 20 Second Spoiler aerodynamic center Aircraft Response airspeed Altitude Change feet altitude loss angle of attack Beechcraft Duke coefficient Airplane control inputs control lift Conventional ILS Approach deg or rad descent rate control Dimensional Stability Derivatives direct lift control evaluation pilots flight path control Flight Research Laboratory flight simulator ft/sec glide slope tracking glideslope handling qualities Instrument Landing System instrument rated landing approach lift coefficient light aircraft Load Factor middle marker modified Cardinal nominal pitching outer marker phugoid excitation phugoid motion Pilot G pitch angle changes Pitch Angle degrees power setting q S b2 Response to 20 RMS error second spoiler pulse shown in Figure shows an approach sp 3C sp sp spdlc speed and pitch Speed Variation feet/second speedbrake Spoiler Deflection degrees spoiler drag spoiler inputs spoiler pitching spoiler system spoilers retracted Stability Derivatives switch trim speed University of Kansas Vertical Speed feet/minute