Control law synthesis for the plane angular motion of a small-sized spacecraft using the direct Lyapunov method
| Authors: Kolesnikova V.E. | Published: 09.04.2025 |
| Published in issue: #2(97)/2025 | |
| DOI: DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: small-sized spacecraft, planar angular motion, terminal control, control law, direct Lyapunov method, Lyapunov candidate function | |
Studying different methods in solving optimization problems of the impulse Earth — Mars interplanetary flights
| Authors: Huang Y.Y. | Published: 20.01.2025 |
| Published in issue: #6(95)/2024 | |
| DOI: DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: space research, interplanetary flight, trajectory optimization, multi-impulse maneuver, genetic algorithm | |
Methods in the forecasting models construction based on the evolutionary algorithms
| Authors: Grigoryev L.V., Stepchenko E.I. | Published: 25.01.2024 |
| Published in issue: #12(89)/2023 | |
| DOI: DOI: 10.18698/2541-8009-2023-12-959 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: inertial navigation system, navigation system, self-organization algorithm, gyro-stabilized platform deflection angle, short-term forecast, unmanned aerial vehicle, inertial navigation system errors, correction | |
Specifics in the positioning systems development for the space technology products
| Authors: Danshin D.A. | Published: 25.01.2024 |
| Published in issue: #12(89)/2023 | |
| DOI: DOI: 10.18698/2541-8009-2023-12-958 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: space technology, positioning system, coordinates, accuracy, actuator, roller mechanism, shell, backlash-free mechanism | |
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 | |