Optimization of multi-mode rendezvous trajectories with constraints

Author:

Ulybyshev Yu. P.

Publisher

Pleiades Publishing Ltd

Subject

Space and Planetary Science,Astronomy and Astrophysics,Aerospace Engineering

Reference15 articles.

1. Navigatsionnoe obespechenie poleta orbital’nogo kompleksa “Salyut-6”—“Soyuz”—“Progress” (Navigation Support for a Flight of the Salyut-6—Soyuz—Progress Orbital Complex) Petrov, B.N. and Bazhinov, I.K., Eds., Moscow: Nauka, 1985.

2. Lidov, M.L., Mathematical Analogy between Some Optimal Problems of Trajectory Correction with Choosing a Set of Measurements and Algorithms of Their Solution, Kosm. Issled., 1971, vol. 8, no. 5, p. 687 (Cosmic Research, pp. 649–664).

3. Bakhshiyan, B.Ts., Nazirov, R.R., and Elyasberg, P.E., Opredelenie i Korrektsiya Dvizheniya (Garantiruyushchii Podkhod) [Determination and Correction of Motion (Guaranteed Approach)], Moscow: Nauka, 1980.

4. Waespy, C.M., Linear Programming for Orbital Transfer Trajectories, Operations Research, 1970, vol. 18, no. 6, pp. 635–653.

5. Lassere, E., Dufour, F., and Bernussou, J.A., A Linear Programming Solution to the Homogenous Satellite Constellation Station Keeping, 48th Intern. Astronautical Congress, Turin (Italy), 1997.

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