2.5 Foward speed, knots. 52 Thrust, Newtons. 795 Mass, kg. 4.19 Length, Meters. 0.5334 Diameter, Meters. 21 Diameter, Inches. 0 x CG offset, Meters. 0.381 Dist from pivot to ring CP, Meters. 15 Dist from pivot to ring CP, In. 0.1196 Control surface Area, Meters^2. 185.3804 Control surface Area, Inches^2. 0.60604 Area of ring and struts, M^2. 4.26 Ring/strut aspect ratio. 0.723 Crossflow drag coefficient 0.0065 Constant component of drag coeff. 0.9 Oswald efficiency factor. 3.392 Coeff. of lift slope. 1.8855 Distance from CG to CP of ring, Meters. 1.5045 Distance from CG to pivot point, Meters. 709.1645 Inertia about (principal) z axis, kg-m^2. 22.619 Inertia about (principal) x axis, kg-m^2. -149.8973 Deriv of N wrto r, kg-m. -632.025 Deriv of N wrto v (Munk Moment), kg. 50.88 Deriv of Y wrto r, kg. -78.7411 Deriv of Y wrto v, kg/m. -636 Deriv of Y wrto v-dot (Added Mass),kg. -567.3316 Deriv of N wrto r-dot (Added Inr),kg-m^2. 0 Deriv of Y wrto r-dot. 0 Deriv of N wrto v-dot. 0 Deriv of Y wrto r|v|. -557.8282 Deriv of Y wrto v|v|. 273.48 Deriv of N wrto v|v|. -983.9755 Deriv of N wrto r|r|. -------------Linear Analysis:------------- Steady-State Values: The rudder angle is 15 Deg. The CG drift angle is 31.8739 Deg. The turn rate is -20.4541 Deg/Sec The turn radius is 3.6026 Meters or 0.85982 vehicle lengths. The control-torque component about the CG is -190.7376 N-m The control-torque component about the pivot point is -34.4033 N-m The total steady-state torque about the CG is 512.7497 N-m The total steady-state torque about the pivot point is 107.7492 N-m The eigenvalues are: evals = -0.1568 -1.0010 The natural frequency, damping ratio, and time constant are: f_n , damping ratio, time constant ans = 0.0250 1.0000 6.3757 0.1593 1.0000 0.9990 -------------Simulation of Nonlinear EOM:------------- Simulation Initialization: MSwayInv [0][0] = 6.988120e-04 MSwayInv [0][1] = -0.000000e+00 MSwayInv [1][0] = 0.000000e+00 MSwayInv [1][1] = 7.833945e-04 P[4] = 7.950000e+02 P[5] = 1.286111e+00 P[6] = -1.885500e+00 P[7] = -1.504500e+00 P[8] = 3.392000e+00 P[9] = 1.697183e-01 P[10] = 6.500000e-03 P[11] = 8.302292e-02 P[12] = 6.147440e+01 P[13] = -7.874105e+01 P[14] = 5.088000e+01 P[15] = 0.000000e+00 P[16] = -5.578282e+02 P[17] = 0.000000e+00 P[18] = -6.320250e+02 P[19] = -1.498973e+02 P[20] = 0.000000e+00 P[21] = 2.734800e+02 P[22] = -9.839755e+02