System implementation of computer-aided design of control-diagnostic and test operations
Authors: Samsonov K.S., Sevryukova A.V., Salakhatdinova A.R., Provatorov A.S. | Published: 28.06.2017 |
Published in issue: #7(12)/2017 | |
DOI: DOI: 10.18698/2541-8009-2017-7-130 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: technical innovations, control and diagnostic tools, computer-aided design |
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 |
A machine vision algorithm for an agricultural unmanned aerial vehicle
Authors: Voronin A.V. | Published: 12.07.2017 |
Published in issue: #8(13)/2017 | |
DOI: DOI: 10.18698/2541-8009-2017-8-151 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: hyperspectral imaging, UAV, NDVI, aerial photography, machine vision, heterogeneous robots, group control, decentralised method |
Flight module and Venus entry vehicle
Authors: Dugin D.A. | Published: 12.07.2017 |
Published in issue: #8(13)/2017 | |
DOI: DOI: 10.18698/2541-8009-2017-8-154 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: spacecraft, flight module, reentry vehicle, aerodynamic characteristics, transmitting antenna, pressurized compartment |
Analysis of experimental investigation techniques for the case of velocity measurement on a ballistic track
Authors: Bogomolova P.D. | Published: 14.09.2017 |
Published in issue: #9(14)/2017 | |
DOI: DOI: 10.18698/2541-8009-2017-9-160 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: velocity estimation techniques, ballistic track, determining the drag coefficient experimentally |
Numerical simulation of combustion processes for hydrogen-air mixture in a variable cross-section pipe
Authors: Korshunova M.R. | Published: 14.09.2017 |
Published in issue: #9(14)/2017 | |
DOI: DOI: 10.18698/2541-8009-2017-9-165 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
Keywords: combustion, hydrogen-air mixture, gas dynamic computation, simulation of combustion in a pipe, reactor-based approach |
Simulating the process of cooling the high temperature flow in experimental ground rigs by means of water injection
Authors: Polyakov K.V. | Published: 04.10.2017 |
Published in issue: #10(15)/2017 | |
DOI: DOI: 10.18698/2541-8009-2017-10-181 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
Keywords: split, diffusion, disintegration model, cooling the high temperature flow |
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 |
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 |
Developing the parameters determination program for defining the trajectory of the sub-orbital re-entry space vehicle of the tourist class
Authors: Kapitonov D.D. | Published: 09.10.2017 |
Published in issue: #10(15)/2017 | |
DOI: DOI: 10.18698/2541-8009-2017-10-186 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: re-entry space vehicle, flight trajectory, pitch angle, angle of attack, flight altitude |