导弹仿真基于matlab导弹轨迹和撞击位置仿真【含Matlab源码 2067期】.zip

# Missile parameters in the following order from left to right: # Missile ID # Initial position in X0, Y0, Z0 coordinate (m) # Initial mass and landing mass: m0 and mf (kg) # Initial thrust magnitude Thmag0 (N) # Direction angle (degree): theta, phi # Burn time Tburn (s) 1 0.12 29999.14 1.54 700 90 100000.00 -41.24 52.01 11.11 2 0.15 0.54 2.54 700 90 101000.00 32.65 53.02 11.05 3 0.10 101.43 2.43 700 90 99000.00 20.18 53.62 11.09 4 0.16 29812.45 2.12 700 90 96000.00 -15.65 50.51 11.13 5 0.11 15432.98 0.15 700 90 90000.00 5.86 49.07 11.02 6 0.14 29934.54 2.24 700 90 85000.00 -25.34 51.52 11.05 7 0.13 212.43 1.23 700 90 80000.00 10.24 50.05 11.98