There are basically 3 
  
tems in use at AFMTC for obtaining mi 
  
>tory data. These 
    
1i, and the Askania 
  
are the Ballistic Camera, the 
Cine-theodolite. 
  
    
amo T es y e^ A nn mani Ter 14400 A - fe Bn oo i 5 7^ 
instruments and are primarily used tc the tial po- 
sition of the misslle along trajectory at | ticular instances 
        
of time. From this position 
    
velocity and acceleration in: the 
a += 4 +13 la 
avuivuae 
    
Fixed Camera and the 
data: the pitch, yaw, and roll, of the missile 
ballistic camera syst 
    
instrumentation system to be 
- 
  
  
x m EN bs des zx » > 5 fL 453^ 1 1 
Systematic error less he random error) can also be 3 
  
as a range calibration syste 
  
    
tematic error from any other of r ation 
This procedure is currently be: used with the Azusa System. 
  
  
e a^ f^* dt EN AV de En À cng 
grammetry. In essence, this 
   
pendent orientation of each camera to be used in the triangu- 
lation net; and second the determination of the most probable 
  
Spatial position by the 
  
each of the separate camera