Optimizing flight trajectories for space vehicles with an additional fuel tank. I

Author:

Grigoriev I. S.,Danilina I. A.

Publisher

Pleiades Publishing Ltd

Subject

Control and Systems Engineering,Electrical and Electronic Engineering

Reference44 articles.

1. Tsentr obrabotki i otobrazheniya poletnoi informatsii GKNPTs im. M.V. Khrunicheva. Proshedshie puski (Khrunichev Center of Processing and Visualization of Flight Information. Past Launches). http://coopi.khrunichev.ru/main.php?id=11

2. Grigor’ev, I.S. and Danilina, I.A., Optimization of Interorbital Three-dimensional Transfer Trajectories for Stage Spacecraft, Autom. Remote Control, 2007, vol. 68, no. 8, pp. 1372–1390.

3. Zenger-Bredt, I., A Study of Optimal Conditions for Vertical Flight of a Rocket with Arbitrary Number of Stages in a Gravity Field, Vopr. Raketnoi Tekh., 1954, no. 5(23), pp. 3–26.

4. Okhotsimskii, D.E. and Eneev, T.M., Some Variational Problems Related to Launching a Man-Made Earth Satellite, Usp. Fiz. Nauk, 1957, vol. 63, no. 1a, pp. 5–32.

5. Troitskii, V.A., Motion Optimization for a Multi-Stage Rocket, Prikl. Mat. Mekh., 1965, vol. 29, no. 4, pp. 745–750.

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