A Mathematical Model of the Interval Control System for the Movement of Spacecraft Links
The structure of the cable tension stabilization system for the weightlessness simulation stand has been developed. Based on it, a mathematical model of the control system for the vertical movement of the spacecraft links has been developed, taking into account the interval uncertainty of the parameters. An algorithm for parametric synthesis of a PI controller based on modal synthesis is proposed. The efficiency of the synthesized control system for the vertical movement of the spacecraft links is confirmed by the results of digital modeling.
Authors
- Tatiana Ezangina (ORCID: https://orcid.org/0000-0002-4948-5972)
- Sergey An. Gayvoronskiy (ORCID: https://orcid.org/0000-0002-7156-2807)
- Maxim Mikhailovich
Institutions
- National Research Tomsk State University (RU)
- Tomsk Polytechnic University (RU)
Publication Details
- Published
- 2024-11-13
- DOI
- https://doi.org/10.1109/summa64428.2024.10803720
- Primary Topic
- Aerospace Engineering and Control Systems
- Type
- article
- Field-Weighted Citation Impact
- 0.00