Abstract
The attitude regulation control of rigid-flexible coupling satellites is investigated in this paper. Firstly a state observer is designed to estimate the vibration speed of the flexible appendage. With the adaptive method used to compensate the disturbance, a predefined-time attitude regulation controller is then proposed, under which the attitude of a rigid-flexible coupling satellite can be drawn to the desired point in predefined time and hold steady. Finally a simulation example is provided to illustrate the effectiveness of the proposed attitude controller.
| Original language | English |
|---|---|
| Title of host publication | 2024 4th International Conference on Electrical Engineering and Control Science, IC2ECS 2024 |
| Publisher | Institute of Electrical and Electronics Engineers Inc. |
| Pages | 765-769 |
| Number of pages | 5 |
| ISBN (Electronic) | 9798331510107 |
| DOIs | |
| State | Published - 2024 |
| Event | 4th International Conference on Electrical Engineering and Control Science, IC2ECS 2024 - Nanjing, China Duration: 27 Dec 2024 → 29 Dec 2024 |
Publication series
| Name | 2024 4th International Conference on Electrical Engineering and Control Science, IC2ECS 2024 |
|---|
Conference
| Conference | 4th International Conference on Electrical Engineering and Control Science, IC2ECS 2024 |
|---|---|
| Country/Territory | China |
| City | Nanjing |
| Period | 27/12/24 → 29/12/24 |
UN SDGs
This output contributes to the following UN Sustainable Development Goals (SDGs)
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SDG 7 Affordable and Clean Energy
Keywords
- attitude regulation control
- predefined-time control
- rigid-flexible coupling satellites
- state observer
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