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. CONSIDER THE KINEMATIC MODEL OF AN AIRPLANE cos ceas WHERE X, Y, Z REPRESENTS PIT, THE POSITION, O,B,ARE THE PITCH, Rogo YAW, AND ROLL
. CONSIDER THE KINEMATIC MODEL OF AN AIRPLANE cos ceas WHERE X, Y, Z REPRESENTS PIT, THE POSITION, O,B,ARE THE PITCH, Rogo YAW, AND ROLL ANGLES RESPECTIVELY, AND U, IS THE INPUT w 2.0.0.-. X. pin B OOOOO 11 0 0 O 1 0 GIVEN: Tools We Vio= 100 ms V = 110 m/s Who = 0.1 RAD/ W,-0 RAD/S MD W20 - 1 Mays W21=0.8 RAD/S Wso = Os W3 = 0.1 RAD's 1) Write the equivalent discrete time system. 2) Perform one step of integration with the Forward Euler and Runge-Kutta methods X)-0 000)0.0 YO=0(6)=1/4 AD 2(0) - 100 0() . CONSIDER THE KINEMATIC MODEL OF AN AIRPLANE cos ceas WHERE X, Y, Z REPRESENTS PIT, THE POSITION, O,B,ARE THE PITCH, Rogo YAW, AND ROLL ANGLES RESPECTIVELY, AND U, IS THE INPUT w 2.0.0.-. X. pin B OOOOO 11 0 0 O 1 0 GIVEN: Tools We Vio= 100 ms V = 110 m/s Who = 0.1 RAD/ W,-0 RAD/S MD W20 - 1 Mays W21=0.8 RAD/S Wso = Os W3 = 0.1 RAD's 1) Write the equivalent discrete time system. 2) Perform one step of integration with the Forward Euler and Runge-Kutta methods X)-0 000)0.0 YO=0(6)=1/4 AD 2(0) - 100 0()
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