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

By D.Subbaram Naidu

The suggestion of aeroassisting for orbital move has been well-known as one of many severe applied sciences for pioneering the distance frontier. In area transportation platforms, aeroassisting (or aerobraking), outlined because the deceleration due to the consequences of atmospheric drag upon a automobile in the course of orbital operations, opens new venture possibilities, specially with reference to the institution of the everlasting area Station Freedom and area explorations to different planets equivalent to Mars. the most components of study mentioned during this monograph are atmospheric access challenge via the tactic of matched asymptotic expansions, coplanar and non-coplanar orbital transfers with aeroassist know-how, orbital plan switch with aerocruise, and neighbouring optimum information. a distinct characteristic is the bibliography as a way to give you the reader with a literature prestige for additional research.

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Extra resources for Aeroassisted Orbital Transfer: Guidance and Control Strategies

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Naidu, "Fuel-optimal trajectories of transfer with plane change," 1EEE Trans. Aerospace and Vol. 27, pp. 361-369, March 1991. @ 1991 IEEE. IEEE is hereby acknowledged.

X. Vinh, "Minimum-fuel aeroassisted coplanar orbit transfer using lift modulation," J. Guidance, Control, and Dynamics, 8, 134-141, 1985. [4] A. Miele, V. K. Basapur, and W. Y. Lee, "Optimal trajectories for aeroassisted coplanar orbit transfer," J. Opt. , 52, 1-24, 1987. [5] M. H. Kaplan, Modern Spacecraft Dynamics and Control, John Wiley & Sons, New York, 1976. [6] J. P. Maree, Optimal Space Trajectories, Elsevier Scientific Publishing Company, Amsterdam, 1979. [7] J. Stoer, and R. Bulirsch, Springer-Verlag, New York, 1980.

Note that in the simplified procedure, any kind of transcendental equations are avoided and explicit solutions are obtained for the composite solution. Moreover, the common solution is very easily obtained by formulating or generating the various terms of the inner limit of the outer expansion as a polynomial in the stretched variable as [14,15], _ _ + girl(h__-O) + hv o(h=O) ] + Vom = VoOa=O) '~: ---- '~o(h=O) + e['~l(h=O ) + ll~o(h=O)] + ...... a m = a (h=O) + e[alOa=O) + fide Oa=O)] + o o o .

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