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Appendix I / Utilities / WGS 84 Target and Missile Data
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Table 22-6 : Missile Kinematics ( Pre-Launch and Post-launch )
SYM UTILITY ARG DEFINITION
M M
TA DC_TO_YPR EA Alignment to Missile LOS axis transform
M
Pm & M_PRODUCT
E
o,
m
P & M_PRODUCT_AT
G
d,
m
P & M_PRODUCT
B
EA & W_TO_DE
B
E & DW_TO_D2E
A
B
C,
B
ω M_ADD
MV
T B YPR_TO_DC
MV
T M M_PRODUCT_BT
B
T M M_PRODUCT_BT
P & V_S_MAG
o,
m
B
m
g M_PRODUCT
B
r,
m
P M_PRODUCT
B
C,
E
ω M_PRODUCT
B
C,
B
ω M_ADD
MV
E M YPR_TO_DC
B
E M YPR_TO_DC
hA
P m V_H_MAG
hA
Pm & V_H_MAG
hG
d,
m
P & V_H_MAG
M
A
A
m
T , P&
Missile velocity wrt (o) in Missile LOS axes
A A
E , Pm
T & Missile velocity wrt (o) in ECEF axes
G E
A o,
m P ,
T & Missile Velocity in LGA axes at (m)
Ε Β
B
A,
B
Α , ω Missile Body angular velocity wrt Align’t axes
B B
A , B A,
B ,ω
ω , Α & Missile Body angular accel’n wrt Alignment axes
ΕΒ
B B
C , E A,
B ,ω
ω Missile inertial angular rate wrt Celestial axes
MV
A
B
A
T , T Missile Body to Velocity axis transform
MV M
A , TA
B M
A , TA
T Missile LOS to Velocity axis transform
G
E
T Missile LOS to Missile Body axis transform
A
Pm & Missile velocity wrt (o)
G
E
ZG
m
T , T , g Gravity wrt (m) in Missile Body axes
B A
E , Pr,
m
T Missile position wrt (r) in Missile Body axes
B
A ,
A
C,
E
T ω Earth’s Siderial rate in Missile Body axes
B
, E
B
A,
B
ω C , ω Missile inertial angular rate in missile body axes
MV
T M Missile velocity orientation wrt missile LOS axes
B
T M
Missile body orientation wrt missile LOS
A
P m Missile horizontal ground range from launcher
A
Pm & Missile horizontal speed in Alignment plane
G
o,
m
M XMV
m N/A o,
m , TS
MV
ξ B ABS_ANG
MV
ξ A
ABS_ANG
MV
ξ M ABS_ANG
B
ξ M ABS_ANG
rB
Po, m
& V_R_MAG
P & Missile velocity over the ground in LGA
V Missile Mach Number
MV
E B
Missile incidence
MV
E A
Missile LOS to velocity vector angle
MV
E M Alignment to missile velocity vector angle
B
E M
Missile LOS to velocity vector angle
B
P & Missile lateral acceleration wrt body axes
o,
m
22.3-8