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Physics ODE
// Euler integration
Fd = ½ρv²·Cd·A
ax = (Fd_x + Fw) / m
ay = (Fd_y / m) − g
x += vx·dt, y += vy·dt
Fd = ½ρv²·Cd·A
ax = (Fd_x + Fw) / m
ay = (Fd_y / m) − g
x += vx·dt, y += vy·dt
TARGET_STATUS: NO_TARGET
ALT_MAX: 0.0 m
RANGE: 0.0 m
VEL_X: 0.0 m/s
VEL_Y: 0.0 m/s
SIM_TIME: 0.0 s
TARGET ELIMINATED
VEL
DRAG
GRAV
AUTO-TRACK
Max Height
— m
Ground Range
— m
Flight Time
— s
Peak Speed
— m/s
Vy / time
Vx / time
Height / dist
Speed / time