Grigoriev Ilia S

Publications in Math-Net.Ru

1. Задача выведения на целевую орбиту космического аппарата максимальной массы с использованием двигателя ограниченной тяги и сбросом отделяемых частей средств выведения в атмосферу Земли
   
   Avtomat. i Telemekh., 2024, no. 1,  21–46
2. Spacecraft transfer optimization with releasing the additional fuel tank and the booster to the Earth atmosphere
   
   Avtomat. i Telemekh., 2023, no. 3,  22–43
3. Optimizing flight trajectories for space vehicles with an additional fuel tank. II
   
   Avtomat. i Telemekh., 2018, no. 2,  135–153
4. Optimizing flight trajectories for space vehicles with an additional fuel tank. I
   
   Avtomat. i Telemekh., 2017, no. 12,  131–140
5. Selection of Perspective Sequences of Asteroids
   
   Avtomat. i Telemekh., 2013, no. 8,  65–79
6. Constructing Pontryagin extremals for the optimal control problem of asteroid fly-by
   
   Avtomat. i Telemekh., 2009, no. 9,  69–84
7. Optimization of interorbital three-dimensional transfer trajectories for stage spacecraft
   
   Avtomat. i Telemekh., 2007, no. 8,  86–105
8. Optimization multiple-turn trajectories of interorbital flights of spacecraft
   
   Keldysh Institute preprints, 2005, 063, 33 pp.
9. Degenerated resonance 4-wave parametric scattering of continuous emission during optical-pumping
   
   Pisma v Zhurnal Tekhnicheskoi Fiziki, 12:7 (1986),  397–400