Attitude control for the rigid spacecraft with the improved extended state observer
In this article, a three-axis attitude manoeuvre spacecraft consisting of a central rigid body and a rotating solar array is studied. The rotating solar array is considered a disturbance to the spacecraft. In the design of the controller, the coupled terms and the rotating solar array are considered...
| Main Authors: | , , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Sciendo
2023-01-01
|
| Series: | Applied Mathematics and Nonlinear Sciences |
| Subjects: | |
| Online Access: | https://doi.org/10.2478/amns.2021.1.00024 |
| _version_ | 1797688789958656000 |
|---|---|
| author | Cao Yuteng Liu Qi He Guiqin Zhao Qiuling Liu Fang |
| author_facet | Cao Yuteng Liu Qi He Guiqin Zhao Qiuling Liu Fang |
| author_sort | Cao Yuteng |
| collection | DOAJ |
| description | In this article, a three-axis attitude manoeuvre spacecraft consisting of a central rigid body and a rotating solar array is studied. The rotating solar array is considered a disturbance to the spacecraft. In the design of the controller, the coupled terms and the rotating solar array are considered a disturbance. The improved extended state observer is proposed by combing the sliding mode observer with the originally extended state observer to estimate the disturbance. The sliding mode control method is adopted to adjust the attitude of the spacecraft. Numerical simulations are presented to demonstrate the outstanding performance of the present observer. |
| first_indexed | 2024-03-12T01:35:46Z |
| format | Article |
| id | doaj.art-0603fa7f91ac449faee4ba27f7e204a6 |
| institution | Directory Open Access Journal |
| issn | 2444-8656 |
| language | English |
| last_indexed | 2024-03-12T01:35:46Z |
| publishDate | 2023-01-01 |
| publisher | Sciendo |
| record_format | Article |
| series | Applied Mathematics and Nonlinear Sciences |
| spelling | doaj.art-0603fa7f91ac449faee4ba27f7e204a62023-09-11T07:01:07ZengSciendoApplied Mathematics and Nonlinear Sciences2444-86562023-01-018112113410.2478/amns.2021.1.00024Attitude control for the rigid spacecraft with the improved extended state observerCao Yuteng0Liu Qi1He Guiqin2Zhao Qiuling3Liu Fang41School of Mechanical Electrical Engineering, Beijing Information Science and Technology University, Beijing100192, China2Beijing Research Institute of Precise Mechatronics and Controls, Beijing100076, China3School of Astronautics, Harbin Institute of Technology, Harbin150001, China1School of Mechanical Electrical Engineering, Beijing Information Science and Technology University, Beijing100192, China1School of Mechanical Electrical Engineering, Beijing Information Science and Technology University, Beijing100192, ChinaIn this article, a three-axis attitude manoeuvre spacecraft consisting of a central rigid body and a rotating solar array is studied. The rotating solar array is considered a disturbance to the spacecraft. In the design of the controller, the coupled terms and the rotating solar array are considered a disturbance. The improved extended state observer is proposed by combing the sliding mode observer with the originally extended state observer to estimate the disturbance. The sliding mode control method is adopted to adjust the attitude of the spacecraft. Numerical simulations are presented to demonstrate the outstanding performance of the present observer.https://doi.org/10.2478/amns.2021.1.00024rigid spacecraftrotating solar arraydisturbanceimproved extended state observersliding mode control |
| spellingShingle | Cao Yuteng Liu Qi He Guiqin Zhao Qiuling Liu Fang Attitude control for the rigid spacecraft with the improved extended state observer Applied Mathematics and Nonlinear Sciences rigid spacecraft rotating solar array disturbance improved extended state observer sliding mode control |
| title | Attitude control for the rigid spacecraft with the improved extended state observer |
| title_full | Attitude control for the rigid spacecraft with the improved extended state observer |
| title_fullStr | Attitude control for the rigid spacecraft with the improved extended state observer |
| title_full_unstemmed | Attitude control for the rigid spacecraft with the improved extended state observer |
| title_short | Attitude control for the rigid spacecraft with the improved extended state observer |
| title_sort | attitude control for the rigid spacecraft with the improved extended state observer |
| topic | rigid spacecraft rotating solar array disturbance improved extended state observer sliding mode control |
| url | https://doi.org/10.2478/amns.2021.1.00024 |
| work_keys_str_mv | AT caoyuteng attitudecontrolfortherigidspacecraftwiththeimprovedextendedstateobserver AT liuqi attitudecontrolfortherigidspacecraftwiththeimprovedextendedstateobserver AT heguiqin attitudecontrolfortherigidspacecraftwiththeimprovedextendedstateobserver AT zhaoqiuling attitudecontrolfortherigidspacecraftwiththeimprovedextendedstateobserver AT liufang attitudecontrolfortherigidspacecraftwiththeimprovedextendedstateobserver |