The optimality of the impulsive Hohmann coplanar elliptic transfer using energy change concepts aggregation of new useful relationships. Part II

• Autorzy: Kamel O. M. , Soliman A. S.
• Języki publikacji: EN

Abstrakty

EN

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.

Słowa kluczowe

EN

orbital mechanics; Hohmann transfer; optimization

PL

mechanika orbitalna; transfer Hohmanna; optymalizacja

• Wydawca: Wydawnictwo Politechniki Łódzkiej
• Czasopismo: Mechanics and Mechanical Engineering
• Rocznik: 2011
• Tom: Vol. 15, nr 1
• Strony: 47--60
• Opis fizyczny: Bibliogr. 10 poz.

Twórcy

autor

Kamel O. M.

autor

Soliman A. S.

• Astronomy and Space Science Dept., Faculty of Sciences, Cairo University, Egypt

Bibliografia

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• [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.