CALVIN
ENGR 315 -
FLIGHT CONTROL DESIGN
Unformatted text preview:
View Full Document
FLIGHT CONTROL DESIGNPROBLEMS:INPUT / OUTPUT TIME DELAYPLANT MODELCLASSICAL 2 DEGREES OF FREEDOMLOOP SHAPING FOR LOOP 4 (YAW RATE)SOLUTIONFLIGHT CONTROL DESIGNUH-60 BLACK HAWKPROBLEMS: COUPLED MOTION IN LONGITUDINAL AND LATERAL AXESCOUPLING OF CONTROL INPUTSINHERENT LOW FREQUENCY INSTABILITY AND BANDWIDTHUNCERTAINTY IN HELICOPTER DYNAMICS AND MATHMATICAL MODELLINGINPUT / OUTPUT TIME DELAYPLANT MODELCLASSICAL 2 DEGREES OF FREEDOMLOOP SHAPING FOR LOOP 4 (YAW RATE)SOLUTIONDYNAMIC DECOUPLING PRECOMPENSATORREDUCES CONTROLLER BANDWIDTHREDUCED PILOT WORKLOADMEETS ADS33D FLIGHT
View Full Document
Unlocking...