Publicou 12 edições por ano
ISSN Imprimir: 1064-2315
ISSN On-line: 2163-9337
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Efficiency of Application of Low-Thrust Throttling Rocket Engines for Near-Earth Orbital Flights
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RESUMO
Research of motion control of spacecraft (SC) with throttling electric rocket engine (ERE) of constant power providing delivery of maximum payload for performing the prescribed interorbital transfer in the central Newtonian gravity field in a given time is under consideration. Efficiency of the optimal control is compared with the computational results, obtained with the use of the classical mathematical model of ideal controllable ERE. The results are obtained in the model problem about SC transfer from a low near-Earth orbit onto the geostationary one. They confirm the adequacy of the constructed mathematical model of the throttling ERE and enable discovering of a number of considerable peculiarities of optimal trajectories.
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Kiforenko B.N., Pasechnik Z.V., Vasiliev I.Yu., Use of equinoctial orbital elements as variables in the problem of minimal time orbit-to-orbit transfer in strong gravitational field under fixed-value thrust, Problemy upravleniya i informatiki, 2003, No 4, 102–114.
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Kiforenko B.N., Pasechnik Z.V., Vasiliev I.Yu., Averaging of motion equations in the problem of optimization with respect to operating speed of interorbital transfer with thrust of constant value in a strong central gravity field, Ibid., 2001, No. 6, 62–76.
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Kiforenko B.N., Pasechnik Z.V., Vasiliev I.Yu., Analytical solutions of the averaged equations of the optimal inter-orbital transfer with constant by magnitude thrust in the strong gravity field, Mezhdunarodnyi nauchno-tekhnicheskiy zhurnal "Problemy upravleniya i informatiki", 2002, No. 2, 126–139.