orbit - x = inv(A'*A)*(A'*r); p = x(1); e = x(2);

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function [p,e] = orbit ([r], [theta]) A = [ones(size(r)) -r.*cos(theta)];
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Unformatted text preview: x = inv(A'*A)*(A'*r); p = x(1); e = x(2);...
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This note was uploaded on 10/11/2011 for the course GEN_ENG 205-1 taught by Professor Nocedal during the Fall '07 term at Northwestern.

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