Analytic solutions for intermediate-thrust arcs of rocket trajectories in a newtonian field

Journal of Applied Mathematics and Mechanics

Volumn 60, Issue 3, 1996, Pages 421-427

  Azimov, D M ^a  

^a NONE

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Indexed keywords

EID: 0030300365     PISSN: 00218928     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0021-8928(96)00053-6     Document Type: Article

References (9)

1. 1. LAWDEN D. F., Optimum Trajectories for Space Navigation. Plenum Press, New York, 1964.
2. 2. AZIZOV A. G. and KORSHUNOVA N. A., The problem of determining the trajectories in a Newtonian field. In Problems of the Mechanics of Controlled Motion. Perm. Gos. Univ., Perm', pp. 5-10, 1984.
3. 3. ROBBINS H. M., Optimality of intermediate-thrust arcs of rocket trajectories. AIAA J. 3, 6, 1094-1098, 1965.
4. 4. ZAVALISHCHIN S. T., A supplement to Lawden's theory. Prikl. Mat. Mekh. 53, 5, 731-738. 1989.
5. 5. AZIZOV A. G. and KORSHUNOVA N. A., The use of the Levi-Civita method to analyse optimum trajectories. Kosmich. Issledovaniya 17, 3, 378-386. 1979.
6. 6. AZIMOV D. M., Spherical trajectories for intermediate-thrust arcs and their application. In Proceedings of the Scientific Conference on "Modelling of Complex Mechanical Systems", Tashkent, 1991.
7. 7. KORSHUNOVA N. A., Optimum rocket trajectories in a central field. In Mechanics and Applied Mathematics. Trudy Tashkent. Gos. Univ., No. 476a, pp. 85-94, 1975.
8. 8. McCUE G. A., Quasilinearization determination of optimum finite-thrust orbital transfers. AIAA J. 5, 4, 755-763, 1967.
9. 9. EHRICKE K., Space Flight, Vol. 2. Nauka, Moscow, 1969.