| Issue |
Section |
Title |
File |
| Vol 5, No 1 (2006) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Control over orbital tether system unfolding |
(Rus)
|
| Vol 6, No 1 (2007) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Approximate methods of calculating optimal flights of space vehicles with low-thrust engines. Part I |
(Rus)
|
| Vol 7, No 1 (2008) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Approximate methods of calculating optimal flights of space vehicles with low-thrust engines. Part II |
(Rus)
|
| Vol 9, No 1 (2010) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Solving the problem of stabilizing program deployment of an orbital tether system taking into account limitations on the rotary motion of the tip body |
(Rus)
|
| Vol 9, No 2 (2010): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Optimization methods of design-ballistic characteristics circumterraneous and interplanetary space vehicle with electrojet engines of low thrust |
(Rus)
|
| Vol 10, No 1 (2011) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Optimal program of controlling continuous low thrust in the flight between noncoplanar elliptical and geostationary orbits |
(Rus)
|
| Vol 11, No 2 (2012) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Assessing the efficiency of flights to high near-earth orbits using boosters with chemical and electro-rocket engines |
(Rus)
|
| Vol 13, No 4 (2014) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Choice of design characteristics of «garbage collector» spacecraft with a low-thrust electrojet engine |
(Rus)
|
| Vol 14, No 4 (2015) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Choosing a program for controlling the deployment of an orbital tether system with deployment speed limitations |
(Rus)
|
| Vol 15, No 1 (2016) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Efficiency of using electric propulsion engines for the task of keeping in a near-circular orbit |
(Rus)
|
| Vol 15, No 1 (2016) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Modeling orbital tether system deployment with limitations on the deployment speed |
(Rus)
|
| 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 16, No 3 (2017) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Influence of turbulence models on calculated values of aircraft aerodynamic properties |
(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 17, No 4 (2018) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Programs of time-optimal control in the problem of rendezvous transfer of spacecraft with low transversal thrust |
(Rus)
|
| Vol 1, No 1 (2002) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Dynamics and motion control of aerospace and space-rocket systems |
(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)
|
