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  316  Figure 4.34. Roll Coupling 