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- [1] Spacecraft Transfer Optimization with Releasing the Additional Fuel Tank and the Booster to the Earth AtmosphereAUTOMATION AND REMOTE CONTROL, 2023, 84 (03) : 211 - 225Grigoriev, I. S.Proskuryakov, A. I.
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- [3] Multi-step optimization strategy for fuel-optimal orbital transfer of low-thrust spacecraftENGINEERING OPTIMIZATION, 2016, 48 (03) : 519 - 542Rasotto, M.Armellin, R.Di Lizia, P.
- [4] Fuel optimization for low-thrust Earth–Moon transfer via indirect optimal controlCelestial Mechanics and Dynamical Astronomy, 2018, 130Daniel Pérez-PalauRichard Epenoy
- [5] Optimization of the transfer trajectory of a low-thrust spacecraft for research of Jupiter using an Earth gravity-assist maneuverSOLAR SYSTEM RESEARCH, 2014, 48 (07) : 606 - 612Konstantinov, M. S.Orlov, A. A.
- [6] Optimization of the transfer trajectory of a low-thrust spacecraft for research of Jupiter using an Earth gravity-assist maneuverSolar System Research, 2014, 48 : 606 - 612M. S. KonstantinovA. A. Orlov
- [7] Fuel optimization for low-thrust Earth-Moon transfer via indirect optimal controlCELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 2018, 130 (02):Perez-Palau, DanielEpenoy, Richard
- [8] Inserting a Maximum-Mass Spacecraft into a Target Orbit Using a Limited-Thrust Engine with Releasing the Separable Part of Its Launch Vehicle into the Earth's AtmosphereAUTOMATION AND REMOTE CONTROL, 2024, 85 (01) : 14 - 32Grigoriev, I. S.Proskuryakov, A. I.
- [9] Low thrust spacecraft transfers optimization method with the stepwise control structure in the Earth- Moon system in terms of the L1-L2 transferINTERNATIONAL CONFERENCE ON MECHANICAL ENGINEERING, AUTOMATION AND CONTROL SYSTEMS 2015 (MEACS2015), 2016, 124Fain, M. K.Starinova, O. L.