COMPUTING INTERCEPT...
Launch CONFIG
Atmosphere PARAMS
Display OPTIONS
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
ROCKETS_ACTIVE: 0
TARGET ELIMINATED
BASE DESTROYED
THE ENEMY MISSILE REACHED YOUR POSITION
VEL
DRAG
GRAV
▮▮ PAUSED
▶ FOLLOWING
AUTO-TRACK
Max Height
— m
Ground Range
— m
Flight Time
— s
Intercepted
0
Vy / time
⛶
Vx / time
⛶
Height / dist
⛶
Speed / time
⛶