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1 Variation of turbulence intensity with altitude Reference 4
4 RQAS Experimental System
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a-gust Power Spectrum actuators AILERON airplane angle of attack automatic disengage BOARD FLAP Cessna 402B Cessna Aircraft comfort rating command model control law control panel control rate weighting cost function Data Frame drive electronics due to a-gust dutch roll Engineer panel flap travel flight computer flight conditions flight software flight test full state feedback gust Hydraulic switch hydraulic system indicator lights INPUT VOLTAGE TBD installed KU-FRL lateral acceleration Limit switches linear model linear simulation locking actuators maneuvering algorithm Master power switch matrices motion sickness nacelle NASA LaRC open loop outboard flaps output weighting Panel switches passenger Pilot panel power spectral densities Power Spectrum Frequency Quality Instrumentation System Ride Quality Ride Quality Augmentation ROLM computer RQAS control surfaces RQAS system rudder sensor package sensor signals separate surface elevator shown in Figure sideslip Signal engage switch Spectrum Frequency rad/sec SURFACE CPT system checkout take-off terminal strip test engineer trim turbulence