NAVWEPS OD-3OT-80 
STABILITY AND CONTROL 
RELATIVELY 
HIGH 
ROLL 
INERTIA 
cc > -I 
RELATIVELY 
y$z> 
0 A /7 
MASS ROLL 
MOTION 
ROLL 
MOTION 
WSITIVE ANGLE 
OF ATTACK. 
ZERO SIDESLIP 
FUSELAGE 
fh SIDEFORCE 
AERODYNAMIC 
AXIS 
FINITE SIDESLIP 
u pgq ROLL 
MOTION 
Figure 4.34. Roll Coupling 
316