Geodesic
Optimal stabilization of the combustion process in liquid rocket motors
Izvestiya Instituta Matematiki i Informatiki Udmurtskogo Gosudarstvennogo Universiteta, Tome 39 (2012) no. 1.

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The problem of optimal stabilization of the combustion process in liquid rocket motors is studied.
Keywords: stabilization, feedback control, delay. 
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A. A. Belov; A. V. Kim. Optimal stabilization of the combustion process in liquid rocket motors. Izvestiya Instituta Matematiki i Informatiki Udmurtskogo Gosudarstvennogo Universiteta, Tome 39 (2012) no. 1. http://geodesic.mathdoc.fr/item/IIMI_2012_39_1_a4/

[1] Crocco L., “Aspects of combustion stability in liquid propellant rocket motors, Part I. Fundamentals – Low frequency instability with monopropellants”, J. Amer. Rocket Soc., 21:6 (1951), 163–176 | MR

[2] Krasovskii N.N., “Analiticheskoe konstruirovanie regulyatorov dlya sistem s posledeistviem”, Prikladnaya matematika i mekhanika, 26 (1962), 39–51 | MR | Zbl

[3] Kim A.V. et al., “Explicit numerical methods and LQR control algorithms for time-delay systems”, Proc. of the Intern. Conf. on Electrical Engineering (Kyungju. Korea, July 21–25, 1998)

[4] Kvon V.Kh., Kim A.V., Kormyshev V.M., Pimenov V.G., Solodushkin S.I., Analiticheskoe konstruirovanie regulyatorov dlya sistem s posledeistviem, UrFU, Ekaterinburg, 2010, 170 pp.

[5] Kim A.V., Volokhova L.E., Zavodnikov D.E., “Lineino-kvadratichnaya stabilizatsiya protsessa sgoraniya topliva v zhidkostnom raketnom dvigatele”, Vestnik Nizhegorodskogo universiteta im. Lobachevskogo, 2011, no. 4(2), 172–173 | MR