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 | |
Optimization of the spacecraft launch into orbit
| Authors: Gorokhov I.E. | Published: 03.09.2020 |
| Published in issue: #7(48)/2020 | |
| DOI: DOI: 10.18698/2541-8009-2020-7-628 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: optimal control, spacecraft, launch into orbit, pitch angle, boundary value problem, geostationary orbit, Pontryagin’s maximum method, system of differential equations, optimality criterion, launch vehicle | |
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 | |
Quadcopter: dynamics and control
| Authors: Lysukho G.V., Maslennikov A.L. | Published: 08.05.2020 |
| Published in issue: #5(46)/2020 | |
| DOI: DOI: 10.18698/2541-8009-2020-5-604 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: UAV, multirotor UAV, quadcopter, mathematical model, control, dynamics, flight dynamics, motors | |
A review of existing methods for reducing the impact area
| Authors: Khukhrina O.I. | Published: 06.04.2020 |
| Published in issue: #3(44)/2020 | |
| DOI: DOI: 10.18698/2541-8009-2020-3-588 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: impact area, disturbing factors, decrease in the impact area, separating parts of launch vehicles, method of burning the separating parts, changing the pitch angle program of the launch vehicle, complementing the design of the separating part by controls, passive stabilization | |
Software implementation of a special module for the study of Venus atmosphere using two spacecraft
| Authors: Zubko V.A., Belyaev A.A. | Published: 19.12.2019 |
| Published in issue: #12(41)/2019 | |
| DOI: DOI: 10.18698/2541-8009-2019-12-555 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: SPICE NAIF, ballistic navigation software, programming, study of Venus atmosphere, radio visibility, translucence zones, Venus, Python, object-oriented programming | |
Unperturbed motion simulation of the navigation satellite constellation
| Authors: Tedeev G.I., Maslennikov A.L. | Published: 18.11.2019 |
| Published in issue: #11(40)/2019 | |
| DOI: DOI: 10.18698/2541-8009-2019-11-551 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: simulation, mathematical model, satellites, satellite constellation, unperturbed motion, global navigation satellite system, GPS, navigation satellites, ODE solving, numerical methods, Runge-Kutta methods | |