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Appendix I / Utilities / WGS 84, Target and Missile Data
_ _
Table 22-5 : Missile Kinematics ( Post-launch )
SYM UTILITY ARG DEFINITION
P o,
m V_S_MAG
B
T A Q_TO_DC
B
E A DC_TO_YPR
B
Po, m
& M_PRODUCT
P & M_PRODUCT
B
o,
m
B
T C M_PRODUCT
M
EA XYZ_TO_YP
&E
M
A DX_TO_DE
&&E
M
A D2X_TO_D2E
M
A,
M
ω DE_TO_W
M
A,
M
ω& D2E_TO_DW
MV
E B XYZ_TO_YP
MV
TB DC_TO_YPR
MV
T A YPR_TO_DC
P
A
P m
Missile range with respect to launcher
B
Q A Alignment to Missile Body axis transform
B
T A
Alignment to Missile Body axis transform
B A
A , Pm
T & Missile Velocity wrt (o) in Missile Body axes
T & missile acceleration wrt (o) in Missile Body axes
B A
A , Pm
A B
C A T ,
T Celestial to Missile Body axis transform
A
P m Missile LOS orientation wrt Alignment axes
A A
m m P ,
P & Missile LOS Euler rates wrt Alignment axes
A
m
, P&
, &P
& Missile LOS Euler accel’n wrt Alignment axes
A
m
M M
A , EA
A
m
E & Missile LOS angular rate wrt Alignment axes
E& & , E&
, E Missile LOS angular accel’n wrt Alignment axes
M
A
M
A
B
o,
m
M
A
P & Missile incidence
MV
E B
Missile Body to Velocity axis transform
MV B
T , T Alignment to Missile Velocity axis transform
B
A
MV MV
EA YPR_TO_DC TA Missile Velocity orientation wrt Alignment axes
The remaining missile parameters are common to both
pre-launch and post launch – see Table 22-6.
22.3-7