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

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Appendix B / Frames of Reference<br />

_ _<br />

the centre of the main RF beam. Y H and Z H span the seeker detector plane<br />

that is bi-normal to X H . When the gimbals are locked, or at rest, the Seeker<br />

Head frame and Missile Body axes are coincident.<br />

m<br />

15.13 Missile Rolled Frame<br />

TARGET SIGHTLINE<br />

MISSILE SEEKER BEAM<br />

MISSILE BORESIGHT<br />

S<br />

ΨB 15-8<br />

H<br />

ΨB<br />

S<br />

X<br />

H<br />

X<br />

B<br />

X<br />

Figure 15-5 : Missile – Target Relative Frames of Reference<br />

The Missile Rolled frame (R) is located at point (m) and is subject to a roll<br />

rotation about X B such that Z R points along the total lateral acceleration<br />

demand vector.<br />

15.14 Target LOS Frame<br />

The Target LOS frame (T) shown in Figure 15-6 is located at point (o). X T<br />

is a vector from (o) through the target at point (t). Z T points upwards and is<br />

normal to the plane spanned by X T and Z A . Y T remains parallel to the plane<br />

spanned by X A and Y A .<br />

15.15 Target Body Frame<br />

The Target Body frame (TB) shown in Figure 15-6 is located at point (t).<br />

X TB points forward along the target’s longitudinal centreline, Y TB right and<br />

Z TB down when the target flies straight and level. Although the target is<br />

t

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