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In this part we investigate all the four feasible configurations for the generalized Hohmann type transfer. We assign the minimized characteristic velocity (Δv1+Δv2)Min by the application of ordinary infinitesimal calculus optimum conditions. By some algebraic manipulations, we determine the independent variables (x)Min. In addition, we considered the analysis relevant to the two parameters x, y relevant to the two impulses at points A, B. It is demonstrated that the elliptic Hohmann type transfer is the most economic one by this new representation.
Czasopismo
Rocznik
Tom
Strony
47--60
Opis fizyczny
Bibliogr. 10 poz.
Twórcy
autor
autor
- Astronomy and Space Science Dept., Faculty of Sciences, Cairo University, Egypt
Bibliografia
- [1] Roy, A.E.: Orbital Motion, Fourth Edition, IOP Publishing Ltd., Bristol and Philadelphia, 2005.
- [2] Prussing, J, E. and Conway, B.A.: Orbital Mechanics, Oxford University Press, 1993.
- [3] Prussing, J. E.: Simple Proof of the Global Optimality of the Hohmann Transfer, Journal of Guidance, Control and Dynamics, pp. 1037-1038, 1992.
- [4] Palmore, J.: An Elementary Proof of the Optimality of Hohmann Transfer, Journal of Guidance, Control and Dynamics, pp. 629-630, 1984.
- [5] Edelbaum, T. N.: How Many Impulses?, Astronautics and Aeronautics, pp. 64-69, 1967.
- [6] Barrar, R.B.: Acta Astronautica, vol. IX / Fasc. 1, pp. 1-11, 1963.
- [7] Marec, J.P.: Space - Vehicle Trajectories: Optimization, Reprinted from System & Contral Encyclopedia, Theory, Technology, Applications, Pergamon Press, 1989.
- [8] Lawden, D.F.: Journal of Guidance, vol. 15, No 3: Engineering Notes, pp. 788-791, 1990.
- [9] Hiller, H.: RAE (Royal Aircraft Establishment), Tech. Note No Space 67, 1964.
- [10] Chobotov, V.A.: Orbital Mechanics, Third Edition, AIAA, Education Series, 2002.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-LOD9-0027-0030