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DOAJ Open Access 2022

ON THE STABILITY OF THE STABILIZED MOTION OF A CARRIER ROCKET WITH A LIQUID-PROPELLANT JET ENGINE AND AN ONBOARD DIGITAL COMPUTER IN THE STABILIZATION LOOP

Eugene Aleksandrov Tetiana Aleksandrova Iryna Kostianyk Yaroslav Morgun
Lihat Sumber DOI

Abstrak

The problem of choosing the values of the variable parameters of the digital stabilizer of the cosmic stage of a carrier rocket with a liquid-propellant jet engine and an onboard digital computer in the stabilization loop, which ensures stable movement of the stage along the entire active section of the flight trajectory, is considered. The effect of the stabilizer quantization period on the stability region of a closed-loop stabilization system is considered. It is recommended to choose the intersection of stability regions corresponding to uniformly distributed moments of time along the active section of the stage flight trajectory as acceptable values for the variable parameters of the stabilizer of a non-stationary stabilization object.

Topik & Kata Kunci

Computer software Information theory

Penulis (4)

E

Eugene Aleksandrov

T

Tetiana Aleksandrova

I

Iryna Kostianyk

Y

Yaroslav Morgun

Format Sitasi

APA MLA BibTeX
Aleksandrov, E., Aleksandrova, T., Kostianyk, I., Morgun, Y. (2022). ON THE STABILITY OF THE STABILIZED MOTION OF A CARRIER ROCKET WITH A LIQUID-PROPELLANT JET ENGINE AND AN ONBOARD DIGITAL COMPUTER IN THE STABILIZATION LOOP. https://doi.org/10.20998/2522-9052.2022.2.05

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Informasi Jurnal
Tahun Terbit
2022
Sumber Database
DOAJ
DOI
10.20998/2522-9052.2022.2.05
Akses
Open Access ✓