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

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

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9.6.2 CLOS Study<br />

The CLOS study showed how important missile longitudinal acceleration<br />

and body-to-beam compensation are, particularly at low speed and when<br />

boosting. The miss distances achieved with the fully compensated guidance<br />

law were 3 times larger than the PN equivalents. A feature of CLOS is the<br />

increase in miss distance with range, hence the need for a seeker and a<br />

terminal guidance phase at long-range.<br />

Under ideal conditions the beam stiffness used allowed the missile to follow<br />

the weaving target LOS indicating, as did PN, that range-to-go bandwidth<br />

control is required if control effort is to be minimised.<br />

9.6.3 Tracking Filter Tuning Study<br />

Velocity, acceleration and Singer filter performance against idealised targets<br />

was investigated; work is ongoing with the weave filter. System noise<br />

levels for the VA filters were set at 1 m 2 /s 4 /Hz and 1 m 2 /s 6 /Hz respectively<br />

to accommodate digitisation errors.<br />

Using the low bandwidth acceleration filter, the normalised acceleration<br />

error rapidly exceeded the expected 3σ error in response to changes in target<br />

acceleration. This is ideal, both for IMM discrimination, and for later<br />

manoeuvre detection. By comparison, when a new constant acceleration<br />

regime is established the filter recovers slowly taking 2 s to 3 s. This is why<br />

the IMM filter transition probabilities are set to inject system noise under<br />

these circumstances.<br />

Changing the measurement processing order made no difference to the<br />

tracking errors using a 10 Hz data rate. Using the most accurate<br />

measurement first, with re-linearisation, is only expected to improve<br />

accuracy at lower data rates.<br />

The low bandwidth Singer filter as expected provided little measurement<br />

filtering with PVA errors of the order of 20 m, 50 m/s and 80 m/s 2 .<br />

However, changes in the target flight regime associated with avoidance<br />

manoeuvring are expected to be short. During such periods the velocity and<br />

acceleration filters remained stable, if inaccurate, when tracking targets with<br />

a different dynamic model.<br />

9-29

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