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

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values of CN are not always a reliable indicator of accuracy, nor even<br />

stability, Daum [D.2] . Noise of 1 m 2 /s 4 /Hz was finally selected. The actual<br />

position and acceleration errors compared with filter expectations are shown<br />

in Figure 9-40. The position error is reasonably matched to the expectation,<br />

although the steady state acceleration error is lower than filter expectation<br />

indicating some over damping.<br />

[metres]<br />

[m/sec**2]<br />

22<br />

20<br />

18<br />

16<br />

14<br />

12<br />

10<br />

8<br />

6<br />

4<br />

10 12 14 16 18 20 22 24 26 28 30<br />

TIME [seconds]<br />

20<br />

18<br />

16<br />

14<br />

12<br />

10<br />

8<br />

6<br />

4<br />

2<br />

9-23<br />

TG_A_MET<br />

TG_A_SIG<br />

TG_P_MET<br />

TG_P_SIG<br />

0<br />

10 12 14 16 18 20 22 24 26 28 30<br />

TIME [seconds]<br />

Figure 9-40 : Tuned Acceleration Filter<br />

Position and Acceleration Errors ( PIP ) and ( PIA )<br />

This performance was compared with that using the Joseph covariance<br />

update, and serially processing combinations of radar range, range-rate and<br />

angle measurements. There was very little improvement in performance at<br />

the current 10 Hz measurement update rate. One concludes that using 64 bit<br />

arithmetic and linearisation between serial measurement updates removes<br />

any sensitivity that may have existed. These techniques, together with<br />

iteration and 2 nd order filtering, are only expected to make a significant<br />

impact if the radar update rate reduces significantly to say 1 Hz.

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