World launch vehicle operations trends
| Authors: Samokhvalova E.A., Shlyakhtenkova A.V. | Published: 15.10.2019 |
| Published in issue: #10(39)/2019 | |
| DOI: DOI: 10.18698/2541-8009-2019-10-536 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: launch vehicle, forecasting, launches, analysis, class, extrapolation, trend model, time series | |
Approach to the development of a mathematical model of the passive trajectory for the separated parts of a space rocket
| Authors: Pachin A.S. | Published: 18.09.2019 |
| Published in issue: #9(38)/2019 | |
| DOI: DOI: 10.18698/2541-8009-2019-9-524 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: mathematical model, passive part of the trajectory, ballistics, space rocket, separating part, measurement information, external factors | |
Study of libration points in the Sun – Venus system in order to form the orbital system for the study of the Venus atmosphere
| Authors: Zubko V.A., Belyaev A.A. | Published: 07.08.2019 |
| Published in issue: #8(37)/2019 | |
| DOI: DOI: 10.18698/2541-8009-2019-8-508 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: limited three-body circular problem, libration points, stability, formation of the orbital system, Sun, Venus, spacecraft, Lyapunov method | |
Development of the aircraft control system in terms of discreteness of input signals on control organs
| Authors: Zabolotskaya E.V., Nikanorova M.D. | Published: 30.05.2019 |
| Published in issue: #5(34)/2019 | |
| DOI: DOI: 10.18698/2541-8009-2019-5-480 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: aircraft, accuracy, control system, discreteness, homing, hit zone, guidance, homing head | |
Numeral calculation of aerodynamic characteristics unmanned aerial vehicle
| Authors: Nikanorova M.D., Zabolotskaya E.V. | Published: 11.04.2019 |
| Published in issue: #4(33)/2019 | |
| DOI: DOI: 10.18698/2541-8009-2019-4-464 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: SolidWorks, Flow Simulation, unmanned aerial vehicle, aerodynamic characteristics, numerical simulation, control system, stabilization system, reliability analysis | |
The development of a complex simulation stand of an air defence guided missile flight angular dynamics
| Authors: Vedenichev I.V., Saitova Z.G. | Published: 01.04.2019 |
| Published in issue: #3(32)/2019 | |
| DOI: DOI: 10.18698/2541-8009-2019-3-458 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: sinulation stand, air defence guided missile, Arduino, MATLAB, Simulink, 3D printer, angular missile dynamics, control system | |
Estimation and compensation of zero drifts of angular velocity sensors in strapdown inertial navigation systems
| Authors: Sadchickov Yu.G. | Published: 16.01.2019 |
| Published in issue: #1(30)/2019 | |
| DOI: DOI: 10.18698/2541-8009-2019-1-423 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: strapdown inertial navigation system, angular velocity sensor, drift, gyroscope, satellite navigation system, Kalman filter, compensation estimation, negative feedback | |
Analysis of the impact of implementation methods of three-parameter approach to modeling the angular dynamics of movement of the aircraft
| Authors: Lysikova V.S. | Published: 04.12.2018 |
| Published in issue: #11(28)/2018 | |
| DOI: DOI: 10.18698/2541-8009-2018-11-410 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: aircraft dynamics, coordinate systems, Euler angles, direction cosine matrix, transition schemes between starting and associated coordinate systems, angular motion of the aircraft, three-parameter approach to modeling, mathematical description of the flight | |
Ballistic analysis of flight planning methods for spacecraft inspecting groups of objects on the geostationary orbit
| Authors: Gnezdova E. K. | Published: 15.11.2018 |
| Published in issue: #11(28)/2018 | |
| DOI: DOI: 10.18698/2541-8009-2018-11-404 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: spacecraft, drift, target fly-around, geostationary orbit, planning algorithm, characteristic speed, inspection order, ballistic support, depth-first search, direct search method | |
Assessment of possibility of photon drive application in order to maintain small spacecraft orbit
| Authors: Gubzhev E.A. | Published: 31.10.2018 |
| Published in issue: #10(27)/2018 | |
| DOI: DOI: 10.18698/2541-8009-2018-10-393 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: photon drive, space garbage, low-orbiting spacecraft, nanosatellite, low orbit, head drag coefficient, atmosphere, orbiting satellite lifetime | |