Monitoring and Early Proactive Control of the Orbital Motion of a Charged Spacecraft

DOI

https://doi.org/10.1109/mlsd61779.2024.10739502
Final published version

The orbital motion of a charged spacecraft in the geomagnetic field is investigated. In order to block the disturbing effect of the Lorentz force on the parameters of the spacecraft's orbit, the mathematical apparatus for early proactive control is built. The proposed PID controller protects the spacecraft's orbit from reversal and shape distortion.

Original language	English
Title of host publication	Proceedings of 2024 17th International Conference on Management of Large-Scale System Development, MLSD 2024
Publisher	Institute of Electrical and Electronics Engineers Inc.
Number of pages	5
ISBN (Print)	9798350375718
DOIs	https://doi.org/10.1109/mlsd61779.2024.10739502
State	Published - 24 Sep 2024
Event	17-я Международная конференция «Управление развитием крупномасштабных систем» (MLSD-24) - Duration: 25 Sep 2024 → 25 Oct 2024

Conference

Conference	17-я Международная конференция «Управление развитием крупномасштабных систем» (MLSD-24)
Period	25/09/24 → 25/10/24

Research areas

Lorentz force, PID controller, computer simulation, electrostatic charge, geomagnetic field, orbital motion, proactive control, resonance, spacecraft

ID: 127562877