About one problem of trajectory optimization-Reference-Cited by-同舟云学术

About one problem of trajectory optimization

Published:2008-06 Issue:3 Volume:46 Page:233-237
ISSN:0010-9525
Container-title:Cosmic Research
language:en
Short-container-title:Cosmic Res

Author:

Grigoriev I. S.,Zapletin M. P.

Publisher

Pleiades Publishing Ltd

Subject

Space and Planetary Science,Astronomy and Astrophysics,Aerospace Engineering

Link

http://link.springer.com/content/pdf/10.1134/S0010952508030064.pdf

Reference4 articles.

1. Fedorenko, R.P., Priblizhennoe reshenie zadach optimal’nogo upravleniya (Approximations in Control Theory), Moscow: Nauka, 1978.

2. Grigoriev, K.G. and Zapletin, M.P., Vertical Start in Optimization Problems of Rocket Dynamics, Kosm. Issled., 1997, vol. 35, no. 4, pp. 363–377. Cosmic Research, p. 339–353.

3. Grigoriev, I.S. and Grigoriev, K.G., Conditions of the Maximum Principle in the problem of Optimal Control over an Aggregate of Dynamic Systems and Their Application to Solution of the Problems of Optimal Control of Spacecraft Motion, Kosm. Issled., 2003, vol. 41, no. 3, pp. 307–331. Cosmic Research, p. 285–309.

4. Grigoriev, I.S. and Grigoriev, K.G., Solving Optimization Problems for the Flight Trajectories of a Spacecraft with a High-Thrust Jet Engine in Impulse Formulation for an Arbitrary Gravitational Field in a Vacuum, Kosm. Issled., 2002, vol. 40, no. 1, pp. 88–111. Cosmic Research, p. 81–103.

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