Search by keyword: "aircraft"
Finding the particles distribution function based on the Fokker — Planck equation for the laser plasma
Authors: Savelyev T.A., Savritskiy A.N., Nazaryan A.M. | Published: 06.12.2023 |
Published in issue: #10(87)/2023 | |
DOI: DOI: 10.18698/2541-8009-2023-10-944 | |
Category: Physics | Chapter: Plasma physics | |
Keywords: laser plasma, electron and ion acceleration, particles collisions, particles interaction, distribution functions, Fokker — Planck equation, Rosenbluth — Trubnikov potentials, aircraft |
Simulation of hydrogen combustion in a supersonic air flow with the assumption of a single-stage chemical reaction
Authors: Miroshnichenko S.A. | Published: 17.02.2022 |
Published in issue: #1(66)/2022 | |
DOI: DOI: 10.18698/2541-8009-2022-1-762 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
Keywords: mathematical model, combustion, hydrogen, supersonic combustion chamber, aircraft, assumption, one-stage chemical reaction, distribution |
Study of a laser gyroscope using the Allan variation method
Authors: Bolotnov A.S., Fomin I.I. | Published: 17.06.2021 |
Published in issue: #5(58)/2021 | |
DOI: DOI: 10.18698/2541-8009-2021-5-702 | |
Category: Instrument Engineering, Metrology, Information-Measuring Instruments and Systems | Chapter: Laser and opto-electronic systems | |
Keywords: navigation systems, gyroscope, Allan variation, dispersion, least squares method, ring laser, mobile complexes, aircraft |
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 |
Building a model of vertical movement of the aircraft carrier deck based on the method of group consideration of arguments
Authors: Zhao Xueting | Published: 07.09.2020 |
Published in issue: #8(49)/2020 | |
DOI: DOI: 10.18698/2541-8009-2020-8-635 | |
Category: Instrument Engineering, Metrology, Information-Measuring Instruments and Systems | Chapter: Instruments and Measuring Methods | |
Keywords: aircraft carrier, aircraft, landing, vertical movement of the deck, forecast, method of group consideration of arguments, algorithm, model building, compensation of deck movement |
Computation of the aerodynamic coefficients of a surface-to-air missile using computational fluid dynamics in SolidWorks Flow Simulation
Authors: Tkachenko E.D., Maslennikov A.L. | Published: 08.06.2020 |
Published in issue: #6(47)/2020 | |
DOI: DOI: 10.18698/2541-8009-2020-6-615 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: aerodynamics, aircraft, missile, aerodynamic coefficients, SolidWorks, Flow Simulation, computational fluid dynamics, computer simulation |
Development of self-organization algorithms for navigation systems correction
Authors: Zhao Yang, Shen Xin | Published: 15.10.2019 |
Published in issue: #10(39)/2019 | |
DOI: DOI: 10.18698/2541-8009-2019-10-538 | |
Category: Informatics, Computer Engineering and Control | Chapter: System Analysis, Control, and Information Processing, Statistics | |
Keywords: aircraft, inertial navigation system, self-organization algorithm, navigation system errors, correction scheme, system, mathematical modeling, Kalman filter |
Method for improving the accuracy of aircraft navigation system using the Kalman filter
Authors: Hu Yuhui, Ma Deng | Published: 03.10.2019 |
Published in issue: #9(38)/2019 | |
DOI: DOI: 10.18698/2541-8009-2019-9-529 | |
Category: Informatics, Computer Engineering and Control | Chapter: System Analysis, Control, and Information Processing, Statistics | |
Keywords: Kalman filter, aircraft, Gaussian white noise, inertial navigation system, GPS, error of navigation systems, forecast, error compensation |
Improving accuracy of assessment navigation system errors with the help of Kalman filter in navigation systems of hybrid nature
Authors: Zhao Xueting | Published: 26.06.2019 |
Published in issue: #6(35)/2019 | |
DOI: DOI: 10.18698/2541-8009-2019-6-495 | |
Category: Instrument Engineering, Metrology, Information-Measuring Instruments and Systems | Chapter: Instruments and Measuring Methods | |
Keywords: Kalman filter, algorithm, estimation accuracy, hybrid system, aircraft, mathematical models, inertial navigation system, satellite navigation system |
Development of the Kalman filter modification for the measuring complex of the aircraft for carrier landing
Authors: Wang Lu | Published: 06.06.2019 |
Published in issue: #6(35)/2019 | |
DOI: DOI: 10.18698/2541-8009-2019-6-485 | |
Category: Instrument Engineering, Metrology, Information-Measuring Instruments and Systems | Chapter: Instruments and Measuring Methods | |
Keywords: aircraft, navigation complex, Kalman filter, inertial navigation system, satellite navigation system, correction, gyrostabilized platforms, modification |