Dynamics, ballistics, aircraft movement control

DEVELOPMENT OF AN ADAPTIVE ALGORITHM FOR DETERMINING THE CHARACTERISTICS OF THE LONGITUDINAL FLIGHT MODE OF AIRCRAFT

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Research article

DOI:

https://doi.org/10.60797/IRJ.2025.152.7

Issue: № 2 (152), 2025

Suggested:

09.12.2024

Accepted:

05.02.2025

Published:

17.02.2025

Rightholder: authors. License: Attribution 4.0 International (CC BY 4.0)

820

Optimizing the trajectory of a spacecraft using an ideally regulated engine in the vicinity of a circular orbit

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Research article

DOI:

https://doi.org/10.60797/IRJ.2024.144.24

Issue: № 6 (144), 2024

Suggested:

27.03.2024

Accepted:

30.05.2024

Published:

17.06.2024

Rightholder: authors. License: Attribution 4.0 International (CC BY 4.0)

973

Modelling of a Small Spacecraft Orientation and Stabilization System

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Review article

Nguen K. N.

DOI:

https://doi.org/10.23670/IRJ.2024.141.65

Issue: № 3 (141), 2024

Suggested:

03.03.2024

Accepted:

14.03.2024

Published:

18.03.2024

Rightholder: authors. License: Attribution 4.0 International (CC BY 4.0)

2140

Complanar Encounter of Two Space Vehicles in a Near-circular Orbit Using a Low Thrust Engine

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Research article

DOI:

https://doi.org/10.23670/IRJ.2024.142.155

Issue: № 4 (142), 2024

Suggested:

15.02.2024

Accepted:

22.03.2024

Published:

17.04.2024

Rightholder: authors. License: Attribution 4.0 International (CC BY 4.0)

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