NAVWEPS 00-801-80 
STABILITY AND CONTROL 
CHANGE IN TAIL LIFT 
RELATIVE WIND 
FROM ANGULAR ROTATION 
CHANGE IN TAIL ANGLE OF 
ATTACK DUE TO PITCHING 
VELOCITY 
co 
!!I 30 
8 
; 20 MANEUVERING STICK 
:: FORCE GRADIENT 
g IO 
w 
I 2 3 4 5 6 7 8 
LOAD FACTOR, n 
(OR G) 
CG POSITION 
% MAC / 
LOAD FACTOR 
Figure 4.15. Maneuvering Stability 
269