NAVWEPS 00-807-80 
STABILITY AND CONTROL 
P, 
RAl ^, 
r%“LL 
O/SEC. 
0 
,/ <EiECT 
0 OF ADDED 
POWER 
BOOST 
V. KNOTS 
4 ROLL .lD 
HELIX 
ANGLE 
pb 
TT 
- 
V, KNOTS 
A 
AILERON ----- DEFLECTlON 
8, 
V.KNOTS 
SPEED CORRESPONDING 
TO LIMIT OF PILOT EFFORT 
TO MAINTAIN MAXIMUM DEFLECTION 
A (3 z 3 is 
1.0 
0 c 5 ELASTIC WING TWISTING 
REVERSAL 
Figure 4.30. Control in Roll 
304