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Thesis - Leigh Moody.pdf - Bad Request - Cranfield University

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Appendix I / Utilities / WGS 84 Target and Missile Data<br />

_ _<br />

Table 22-4 : Missile Kinematics (Pre-launch)<br />

SYM UTILITY ARG DEFINITION<br />

P o,<br />

m V_S_MAG<br />

B<br />

T A Q_TO_DC<br />

B<br />

E A DC_TO_YPR<br />

B<br />

Po, m<br />

& M_PRODUCT<br />

P & M_PRODUCT<br />

B<br />

o,<br />

m<br />

B<br />

T C M_PRODUCT<br />

M<br />

EA N/A<br />

A<br />

P m YP_TO_XYZ<br />

M<br />

EA & M_IMAGE<br />

M<br />

E & M_IMAGE<br />

A<br />

M<br />

A,<br />

M<br />

ω M_IMAGE<br />

M<br />

A,<br />

M<br />

ω& M_IMAGE<br />

MV<br />

E B M_ZERO<br />

MV<br />

E A M_IMAGE<br />

MV<br />

TB DC_TO_YPR<br />

MV<br />

T A DC_TO_YPR<br />

A<br />

P m<br />

Missile range with respect to launcher<br />

B<br />

Q A Alignment to Missile Body axis transform<br />

B<br />

T A<br />

Alignment to Missile Body axis transform<br />

B A<br />

A , Pm<br />

T & Missile Velocity wrt (o) in Missile Body axes<br />

T & Missile acceleration wrt (o) in Missile Body axes<br />

B A<br />

A , Pm<br />

A B<br />

C A T ,<br />

T Celestial to Missile Body axis transform<br />

o, m<br />

M<br />

A<br />

Missile LOS orientation wrt Alignment axes<br />

P , E Missile position wrt (o) in Alignment axes<br />

B<br />

EA & Missile LOS Euler rate wrt Alignment axes<br />

E & Missile LOS Euler accel’n wrt Alignment axes<br />

B<br />

A<br />

B<br />

A,<br />

B<br />

ω Missile LOS angular rate wrt Alignment axes<br />

B<br />

A,<br />

B<br />

ω& Missile LOS angular accel’n wrt Alignment axes<br />

22.3-6<br />

Missile incidence<br />

B<br />

E A Missile Velocity orientation wrt Alignment axes<br />

MV<br />

E B Missile Body to Missile Velocity axis transform<br />

MV<br />

E A Alignment to Missile Velocity axis transform<br />

The remaining missile parameters are common to both<br />

pre-launch and post launch – see Table 22-6.

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