D.Subbaram Naidu's Aeroassisted Orbital Transfer: Guidance and Control PDF

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Mo = ~o(h--O) + e[~lOl=O ) + ~o01--0)] + ...... 1~o = IOa=O) + e[Ii(h=O) + l~I (11=0)] + ......... o Here the dot denotes differentiation with respect to the independent variable h. Note that this is also called the intermediate solution in singular perturbation methods [14, 15]. Now force the outer solution (7) to satisfy the given initial conditions, vi, ~/i cti' f~i' and I i corresponding to h = h i. This gives C 1 -- y/21 " I/(l+h) c2 = c┬░sVl+hi i CHAPTER 2: ATMOSPHERIC ENTRY PROBLEM I C 3 = o~i - c o s -i C =t~ 4 COS2Yi (l+hi)vi- 1 .

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Aeroassisted Orbital Transfer: Guidance and Control Strategies by D.Subbaram Naidu


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