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The horizontal and vertical motion of the center of mass of an airplane in the vertical plane can be described using a two degrees of freedom (2 DOF) model. flight path. horizontal You will learn in Aircraft Stability and Control that the equations of motion of the aircraft can be written as I sin y (T D cos y) y) Locos y (T D sin where z is altitude and x is the horizontal distance travelled. Other parameters in the equations are horizontal velocity T thrust D-drag Va vertical velocity m aircraft mass g gravity r flight path angle Lift, drag, and flight path angle are determined by: i 72 SCD pr tan where v and are components of flight speed V in the x and z directions. Note that: The horizontal and vertical motion of the center of mass of an airplane in the vertical plane can be described using a two degrees of freedom (2 DOF) model. flight path. horizontal You will learn in Aircraft Stability and Control that the equations of motion of the aircraft can be written as I sin y (T D cos y) y) Locos y (T D sin where z is altitude and x is the horizontal distance travelled. Other parameters in the equations are horizontal velocity T thrust D-drag Va vertical velocity m aircraft mass g gravity r flight path angle Lift, drag, and flight path angle are determined by: i 72 SCD pr tan where v and are components of flight speed V in the x and z directions. Note that