Lagrangian points in Mars-Phobos system
| Authors: Askerova A.A., Stolbova V.A. | Published: 17.10.2018 |
| Published in issue: #10(27)/2018 | |
| DOI: DOI: 10.18698/2541-8009-2018-10-388 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: libration points, three-body problem, gravitational interaction, gravitational astronomy, aerospace, Mars, stationary position, balance state | |
Analytic investigation of the approaches to increasing the navigational accuracy of the pulse-corrected aircraft
| Authors: Vedenichev I.V. | Published: 24.07.2018 |
| Published in issue: #7(24)/2018 | |
| DOI: DOI: 10.18698/2541-8009-2018-7-341 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: ballistic analysis, pulse correction, accuracy increase, corrected missile, low trajectory, high trajectory, MATLAB, Simulink, flight simulation | |
Localization of the object by means of its acoustic signal
| Authors: Troshina E.Yu. | Published: 18.06.2018 |
| Published in issue: #6(23)/2018 | |
| DOI: DOI: 10.18698/2541-8009-2018-6-331 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: acoustic direction finder, correction function, identifying the position, mathematical model, sound source, miniature microphones, broadband signal, signal delay | |
Selecting the loop gains of the unmanned aerial vehicle pitch attitude control system with allowance for tolerances on the aerodynamic and mass centering characteristics
| Authors: Fam Suan Chyong | Published: 28.05.2018 |
| Published in issue: #5(22)/2018 | |
| DOI: DOI: 10.18698/2541-8009-2018-5-317 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: unmanned aerial vehicle, flight control system, attitude control system, stabilization law, cruise missile, Kharitonov theorem, D-partitioning method, robust stability | |
Materials flux flattening in magnetron spraying systems
| Authors: Greshilov V.V. | Published: 09.10.2017 |
| Published in issue: #10(15)/2017 | |
| DOI: DOI: 10.18698/2541-8009-2017-10-185 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: magnetron spraying system, thin films, masking profiles | |
Using the MATLAB.SIMULINK software suite for ballistic analysis
| Authors: Nikanorova M.D., Vedenichev I.V. | Published: 04.10.2017 |
| Published in issue: #10(15)/2017 | |
| DOI: DOI: 10.18698/2541-8009-2017-10-183 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: MATLAB.Simulink environment, ballistics, numerical simulation, correcting filters | |
Specifics of measuring trajectory velocity of small aircraft by means of optical chronographs
| Authors: Bogomolova P.D. | Published: 12.07.2017 |
| Published in issue: #8(13)/2017 | |
| DOI: DOI: 10.18698/2541-8009-2017-8-149 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: optical chronograph, velocity measurement, drag coefficient, trajectory velocity, ballistic track | |
Launch rockets potential analysis in their orbital injection
| Authors: Stepanova S.V., Zamyatin D.A. | Published: 28.06.2017 |
| Published in issue: #7(12)/2017 | |
| DOI: DOI: 10.18698/2541-8009-2017-7-121 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: launch rocket, spacecraft, rocket and space system, low Earth orbit | |
Computing aerodynamic properties for a model of a detachable fairing flap at a supersonic incident flow velocity
| Authors: Slobodyanyuk D.M. | Published: 26.04.2017 |
| Published in issue: #5(10)/2017 | |
| DOI: DOI: 10.18698/2541-8009-2017-5-101 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: aerodynamic properties, SolidWorks software package, ANSYS software package, thin-walled shells, detachable parts, flow modeling | |
Numerical modeling of aerodynamic wind tunnel experiment
| Authors: Marashan М.V. | Published: 14.03.2017 |
| Published in issue: #5(5)/2016 | |
| DOI: DOI: 10.18698/2541-8009-2016-5-46 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: aerodynamic experiment, wind tunnel, numerical simulation, Solid Works Flow Simulation | |