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guidance, flight mechanics and trajectory optimization

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M<br />

Since 3t does not depend on u explicitly, the control u which minimizes<br />

the bracketed quantity in Eq. (2.4.155) also minimizes the quantity<br />

c n JE {(r,u) ti&x,u,<br />

i=l aq<br />

6 (Y,ULRIZ,Ll) l Let<br />

, or alternately, maximizes the quantity<br />

the p vector be defined by<br />

Then, it follows that the optimal control is that control in the set which<br />

maximizes $a 73;E(xau) - wd. Thus, condition (1) of the<br />

Maximum Principle is satisfied. With the definition of Eq. (2.4.157). the<br />

boundary condition in Eq. (2.4.156) is<br />

And since from(2.4.1561<br />

7; t f

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