Author Details
Храмов, А. А., Самарский национальный исследовательский университет имени академика С.П. Королёва, Russian Federation
Issue | Section | Title | File |
Vol 16, No 3 (2017) | AIRCRAFT AND SPACE ROCKET ENGINEERING | Optimization of space vehicle trans-atmospheric motion by using the method of sequential linearization |
(Rus) |
Vol 17, No 1 (2018) | AIRCRAFT AND SPACE ROCKET ENGINEERING | Optimizing a vehicle trans-atmospheric motion using Pontryagin’s maximum principle |
(Rus) |
Vol 17, No 2 (2018) | AIRCRAFT AND SPACE ROCKET ENGINEERING | Optimization of space vehicle combined orbital plane change maneuver on the basis of the successive linearization method |
(Rus) |
Vol 18, No 1 (2019) | AIRCRAFT AND SPACE ROCKET ENGINEERING | Optimization of space vehicle combined orbital plane change maneuver on the basis of pontryagin’s maximum principle |
(Rus) |
Vol 18, No 4 (2019) | AIRCRAFT AND SPACE ROCKET ENGINEERING | Application of differential evolution algorithm in the problem of aeroassisted orbital plane change maneuver |
(Rus) |