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

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Chapter 6 / Missile Guidance<br />

_ _<br />

Table 6-1 : B-Spline Coefficients and Knots for the Missile Drag Coefficient<br />

{ ( ) ( ) ( ) ( ) ( ) }<br />

λi = 00 05 07 10 40<br />

1x4 1x3 1x3 1x3 1x4 . , . , . , . , . : missile speed<br />

{ ( 00) ( 80 ) ( 160 ) ( 240 ) }<br />

µ j = ° ° °<br />

1x4 1x2 1x2 1x4 . , . , . , . : missile total incidence<br />

CD ij COAST BOOST CD ij COAST BOOST<br />

C(1,1) 0.3493319 0.2993031 C(4,5) 0.8409478 0.8049040<br />

C(1,2) 0.3803946 0.3148281 C(4,6) 1.2111871 1.1439404<br />

C(1,3) 0.3452788 0.3138402 C(4,7) 1.3898173 1.3352739<br />

C(1,4) 0.6622032 0.5781340 C(4,8) 1.5801607 1.5049016<br />

C(1,5) 0.8109929 0.7893868 C(5,1) 0.3505760 0.3017886<br />

C(1,6) 1.1680494 1.1117658 C(5,2) 0.3419176 0.3148543<br />

C(1,7) 1.3330413 1.2874194 C(5,3) 0.4104381 0.3112649<br />

C(1,8) 1.5102555 1.4548981 C(5,4) 0.6495311 0.5846278<br />

C(2,1) 0.3515963 0.2990082 C(5,5) 0.8445568 0.8141522<br />

C(2,2) 0.3144293 0.3169243 C(5,6) 1.2237409 1.1605085<br />

C(2,3) 0.4583260 0.3109562 C(5,7) 1.3993285 1.3571013<br />

C(2,4) 0.5930083 0.5824756 C(5,8) 1.5952919 1.5217631<br />

C(2,5) 0.8719022 0.7891385 C(6,1) 0.3505762 0.3017887<br />

C(2,6) 1.1960613 1.1130887 C(6,2) 0.3419177 0.3148545<br />

C(2,7) 1.3293432 1.2877475 C(6,3) 0.4104383 0.3112650<br />

C(2,8) 1.5322301 1.4624298 C(6,4) 0.6495315 0.5846281<br />

C(3,1) 0.3499098 0.2994020 C(6,5) 0.8445572 0.8141526<br />

C(3,2) 0.3545203 0.3139365 C(6,6) 1.2237415 1.1605090<br />

C(3,3) 0.3921494 0.3150202 C(6,7) 1.3993292 1.3571019<br />

C(3,4) 0.6509853 0.5757280 C(6,8) 1.5952927 1.5217638<br />

C(3,5) 0.8287587 0.7776473 C(7,1) 0.3501669 0.3067943<br />

C(3,6|) 1.1894513 1.1279875 C(7,2) 0.3429002 0.3282534<br />

C(3,7) 1.3818884 1.3024914 C(7,3) 0.4083936 0.3113138<br />

C(3,8) 1.5521059 1.4769744 C(7,4) 0.6535436 0.6007590<br />

C(4,1) 0.3503882 0.2992947 C(7,5) 0.8500621 0.8303082<br />

6-8

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