Category: Aircraft Dynamics, Ballistics, Motion Control, chapter: Aviation and Rocket-Space Engineering | Engineering Journal: Science and Innovation

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Published: 29.06.2022

Authors: Kazakov G.V., Koryanov V.V.

Published in issue: #6(126)/2022

DOI: 10.18698/2308-6033-2022-6-2188

Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control

One-parameter adaptation of an aircraft homing system

Published: 29.06.2022

Authors: Klishin A.N., Kolesnikova D.S.

Published in issue: #6(126)/2022

DOI: 10.18698/2308-6033-2022-6-2187

Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control

Deflection of structural elements in estimating parameters of the controlled motion of the descent vehicle with an inflatable braking device

Published: 25.04.2022

Authors: Koryanov V.V., Kukharenko A.S.

Published in issue: #4(124)/2022

DOI: 10.18698/2308-6033-2022-4-2174

Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control

Planning process to ensure the intended use of the optical telescopes system on board the Russian segment of the International Space Station: implementation features

Published: 21.03.2022

Authors: Toporkov A.G., Belyaev A.M.

Published in issue: #3(123)/2022

DOI: 10.18698/2308-6033-2022-3-2165

Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control

Aspects of applying combined mass–time functional in solving the problem of optimizing the multiple-burn transfer of a spacecraft into a high-energy orbit

Published: 21.03.2022

Authors: Kiriliuk E.V., Stepanov M.N.

Published in issue: #3(123)/2022

DOI: 10.18698/2308-6033-2022-3-2164

Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control

End-to-end optimization of a payload transfers into the geostationary orbit using the combination of the upper stage energy capabilities and the spacecraft own propulsion system

Published: 22.02.2022

Authors: Kiriliuk E.V.

Published in issue: #2(122)/2022

DOI: 10.18698/2308-6033-2022-2-2155

Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control

Determining binocular lenses orientation using inertial sensors: problem solution

Published: 22.02.2022

Authors: Latonov V.V., Belyakov N.V., Petrov A.A., Semenikhin T.A.

Published in issue: #2(122)/2022

DOI: 10.18698/2308-6033-2022-2-2154

Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control

Development of an algorithmic method for improving the landing safety of a damaged heavy transport aircraft

Published: 22.02.2022

Authors: Kostiukov V.M., Tran V.C., Nguyen N.M.

Published in issue: #2(122)/2022

DOI: 10.18698/2308-6033-2022-2-2151

Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control

An automated algorithm approbated for the analysis of telemetric parameters of the state of spacecraft onboard systems

Published: 19.01.2022

Authors: Abanin O.I.

Published in issue: #1(121)/2022

DOI: 10.18698/2308-6033-2022-1-2149

Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control

A global atmosphere model in flight performance assessment and building the reach line when preparing flight missions for sea-based unmanned aerial vehicles

Published: 19.01.2022

Authors: Filippov R.N., Ivanov Yu.A., Kurbatov D.V., Kornilov A.A.

Published in issue: #1(121)/2022

DOI: 10.18698/2308-6033-2022-1-2148

Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control