Question: This is Mathematical Modeling problem~ plz solve it Quwtion 2: An aircraft ying in near steady-state conditions obeys the following lin- earised equations, (11* _
This is Mathematical Modeling problem~
plz solve it

Quwtion 2: An aircraft ying in near steady-state conditions obeys the following lin- earised equations, (11* _ Zn u (in =Xug'r dt mU 1 dt m. 1 where m is the mass of the aircraft, 9 is acceleration due to gravity, 2,, is a lift coefcient, X,1 is a drag coefcient, U is the steady-state speed, 16 is the climb angle, and u is the diemnce between the steady-state speed and the current speed. We can approximate Z" by 2mgf U , and we know X,1
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