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

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Chapter 6 / Missile Guidance<br />

_ _<br />

F3(S)<br />

(WE^3 - WE*WW^2)s 2-(2*WE^2*WW^2)s<br />

s 3+2*WEs 2+(2*WE^2+WW^2)s+(WE^3+WE*WW^2)<br />

TARGET<br />

NOISE<br />

+<br />

P_OM<br />

+<br />

3<br />

MISSILE DYNAMICS T(S)<br />

F2(S)<br />

ANGULAR<br />

GLINT<br />

+<br />

(2*V_OM^2 - A_OM*P_OM)<br />

V_OM<br />

2*WE^2s 2+(WE^3<br />

- WE*WW^2)s<br />

s 3+2*WEs 2+(2*WE^2+WW^2)s+(WE^3+WE*WW^2)<br />

+<br />

WG/P_OM<br />

s+WG<br />

2<br />

F1(S)<br />

2*WEs 2+2*WE^2s+(WE^3<br />

+ WE*WW^2)<br />

s 3+2*WEs 2+(2*WE^2+WW^2)s+(WE^3+WE*WW^2)<br />

+<br />

FF_SW<br />

0<br />

TARGET<br />

LATAX<br />

6-22<br />

STABILITY<br />

LOOP<br />

+<br />

-<br />

1<br />

s<br />

1<br />

s<br />

1/P_OM<br />

10<br />

1<br />

TARGET<br />

DYNAMICS T(S)<br />

MISS<br />

DISTANCE<br />

P_OM<br />

+<br />

+<br />

(2*V_OM^2 - A_OM*P_OM)<br />

V_OM<br />

1<br />

+<br />

Figure 6-3 : Idealised 2D CLOS Simulation<br />

F1(S)_MS<br />

MISSILE<br />

NOISE<br />

+<br />

2*WEs 2+2*WE^2s+(WE^3<br />

+ WE*WW^2)<br />

s 3+2*WEs 2+(2*WE^2+WW^2)s+(WE^3+WE*WW^2)<br />

1/P_OM<br />

4

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