Flight Data
ALT
0 m
SPD
0 m/s
VSPD
0 m/s
AoA
0°
THR
0%
DIST
0 m
TGT
---
TGT DIST
---
TGT BRG
---
THR
STALL
PRE-LAUNCH
Hold SPACE to charge launch
CHASE CAM
W/S: Pitch · A/D: Roll
Q/E: Yaw · Shift/Ctrl: Throttle
C: Camera · R: Recording
T: Cycle Target · L: Aero Lab
SPACE: Launch
HOLD SPACE TO LAUNCH
REC GROUND CAM
MAP
AERODYNAMICS LAB
LIFT
L = ½ρv²SC
L
(α)
ρ=
1.225
v=
0
S=
0.45
C
L
=
0
▲
L =
0
N
DRAG
D = ½ρv²SC
D
C
D
= C
D0
+ C
L
²/(πARe)
C
D0
=
0.030
AR=
5.0
e=
0.80
C
D
=
0
◀
D =
0
N
THRUST
T = T
max
· δ
t
· η(v)
T
max
=
35
δ
t
=
0
η=
0
▶
T =
0
N
WEIGHT
W = mg
m=
2.0
kg
g=
9.81
▼
W =
19.6
N
DYNAMIC PRESSURE
q = ½ρv² =
0
Pa
NET FORCE
F
net
=
0
N accel =
0
m/s²
C
L
vs α — STALL CURVE
■ LIFT
■ DRAG
■ THRUST
■ WEIGHT
CRASHED
Press SPACE to restart
MISSION COMPLETE
DRONE RECOVERED
Press SPACE to restart