Numerical simulation of the combustion products flow of energy condensed material in the flow path considering the erosion effect
Authors: Gogol D.V., Koptev I.I. | Published: 16.02.2023 |
Published in issue: #1(78)/2023 | |
DOI: DOI: 10.18698/2541-8009-2023-1-860 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: power condensed matter, computational fluid dynamics, intra-ballistic characteristics, numerical simulation, ablative coating, power propulsion plant, high-temperature combustion products, flow losses |
Determination of the optimal system of shock waves in the air intake taking into account the dissociation of the incoming air molecules
Authors: Bugay V.V., Shostov A.K. | Published: 15.02.2023 |
Published in issue: #1(78)/2023 | |
DOI: DOI: 10.18698/2541-8009-2023-1-857 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: mach number, shock wave, air intake, supersonic flow, mathematical modeling, maximum total pressure, dissociation of molecules, deceleration parameters |
Characteristics analysis and drive type selection for aileron control of a heavy unmanned aerial vehicle
Authors: Radetskaya A.A. | Published: 22.11.2022 |
Published in issue: #10(75)/2022 | |
DOI: DOI: 10.18698/2541-8009-2022-10-833 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: heavy unmanned aerial vehicle, ailerons, electromechanical drive, electrohydraulic drive, autopilot, characteristics, steering surface |
Designing a database of Russian small spacecraft launches to collect information on space debris
Authors: Pasynkov A.A., Sveshnikova A.S., Titov O.G. | Published: 24.06.2022 |
Published in issue: #6(71)/2022 | |
DOI: DOI: 10.18698/2541-8009-2022-6-799 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: databases, launches, spacecraft, satellite, space debris, forecasting, trend model |
Analysis and comparison of methods for predicting launches of satellites of various types into low Earth orbit
Authors: Pasynkov A.A., Sveshnikova A.S., Titov O.G. | Published: 18.02.2022 |
Published in issue: #2(67)/2022 | |
DOI: DOI: 10.18698/2541-8009-2022-2-767 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: forecasting, launches, spacecraft, satellite, trend model, time (dynamic) series, regression analysis |
Features of the use of Earth’s gravity models in applied problems of ballistics
Authors: Kolesnikova D.S. | Published: 23.09.2021 |
Published in issue: #9(62)/2021 | |
DOI: DOI: 10.18698/2541-8009-2021-9-737 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: total vector of gravitational field strength, anomalous gravitational field, general terrestrial ellipsoid, Krasovsky ellipsoid, Cleraud ellipsoid, model of the Earth’s figure, mathematical modeling, trajectory of an aircraft |
Features of hypersonic aircraft use
Authors: Vafina E.A. | Published: 08.07.2021 |
Published in issue: #6(59)/2021 | |
DOI: DOI: 10.18698/2541-8009-2021-6-710 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: hypersonic aircraft, control, controllability, control methods, maneuvering, missile technology, weapons, control process, control efficiency |
Anomalies of the Earth’s gravitational field in applied problems of ballistics
Authors: Kolesnikova D.S. | Published: 08.07.2021 |
Published in issue: #6(59)/2021 | |
DOI: DOI: 10.18698/2541-8009-2021-6-709 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: full vector of the gravitational field strength, anomalous gravitational field, Earth ellipsoid, Krasovsky ellipsoid, central gravitational field, model of the Earth’s figure, mathematical modeling, trajectory of an aircraft |
Investigation of the movement of the descent vehicle in the planet’s atmosphere taking into account the asymmetry
Authors: Kukharenko A.S. | Published: 27.04.2021 |
Published in issue: #4(57)/2021 | |
DOI: DOI: 10.18698/2541-8009-2021-4-691 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: descent vehicle, differential equations, stable motion, oscillations, coordinate system, damping moment, angle of attack, rotational motion |
Development of a knowledge base for an intelligent aircraft control loop
Authors: Babichenko А.А., Babichenko О.А., Borodaev N.V. | Published: 19.10.2020 |
Published in issue: #9(50)/2020 | |
DOI: DOI: 10.18698/2541-8009-2020-9-641 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: flight and navigation complex, artificial intelligence, expert system, knowledge base, control, aircraft, autonomous testing, rule table, state diagram |