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Qu (4) A simplified landing gear system on airplane shown comprises of masses, springs and viscous dampers. Assuming the system can be modeled as a 2nd order system described as RUNNION AXLE TRUNNION BEAM 6 AUKILIARY SHocK ABSORBER 2 MAIN SHOCK ABSORBER ! DRAG/STDE STRUTss WHEEL AXLE PRIMARY STS SLIDING PISTON ORALTERNATE MID WHEEL AXLE 3 dy+12+100y 450u dt /o dt TRUCK BEAM MID WHEEL AXLE4 (a) Determine the system TF (b) Determine the system poles and WHEEL AXLE and show on the s-plane. (c) Determine the system parameters ς, ω,i, and k (d) By determining the parameters such as TP , do, , %0S, T, , Td etc., sketch the dynamic response of the system.

engineering   Mechanical-Engineering   
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Solution Given dlato as Cakulating the TF toplace bve aion en both sides d O VCs ) - 450 5%, I 2 S +100-7) 201 ·ラ 2-11025 L0 Ta 10 d Oo. 42 Sec

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