Study on the Attitude Control of Spacecraft Using Reaction Wheels
Attitude determination and control of satellite is important component which determines the accomplish satellite missions. In this study, attitude control using reaction wheels and momentum dumping of wheels are considered. Attitude control law is designed by Sliding control and LQR. Attitude maneuv...
| Main Authors: | , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
The Korean Space Science Society
1998-06-01
|
| Series: | Journal of Astronomy and Space Sciences |
| Online Access: | http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/1998/v15n1/OJOOBS_1998_v15n1_245.pdf |
| _version_ | 1827392112582197248 |
|---|---|
| author | Ju-Young Du Kyu-Hong Choi Sanguk-Lee |
| author_facet | Ju-Young Du Kyu-Hong Choi Sanguk-Lee |
| author_sort | Ju-Young Du |
| collection | DOAJ |
| description | Attitude determination and control of satellite is important component which determines the accomplish satellite missions. In this study, attitude control using reaction wheels and momentum dumping of wheels are considered. Attitude control law is designed by Sliding control and LQR. Attitude maneuver control law is obtained by Shooting method. Wheels momentum dumping control law is designed by Bang-Bang control. Four reaction wheels are configurated for minimized the electric power consumption. Wheels control torque and magnetic moment of magnetic torquer are limited. |
| first_indexed | 2024-03-08T17:25:17Z |
| format | Article |
| id | doaj.art-0a38e43b899d4346bcc57bb584216496 |
| institution | Directory Open Access Journal |
| issn | 2093-5587 2093-1409 |
| language | English |
| last_indexed | 2024-03-08T17:25:17Z |
| publishDate | 1998-06-01 |
| publisher | The Korean Space Science Society |
| record_format | Article |
| series | Journal of Astronomy and Space Sciences |
| spelling | doaj.art-0a38e43b899d4346bcc57bb5842164962024-01-02T19:57:17ZengThe Korean Space Science SocietyJournal of Astronomy and Space Sciences2093-55872093-14091998-06-01151245250Study on the Attitude Control of Spacecraft Using Reaction WheelsJu-Young Du0Kyu-Hong Choi1Sanguk-Lee2Department of Astronomy, Yonsei UniversityDepartment of Astronomy, Yonsei UniversityKorea Electronics and Telecommunications Research InstituteAttitude determination and control of satellite is important component which determines the accomplish satellite missions. In this study, attitude control using reaction wheels and momentum dumping of wheels are considered. Attitude control law is designed by Sliding control and LQR. Attitude maneuver control law is obtained by Shooting method. Wheels momentum dumping control law is designed by Bang-Bang control. Four reaction wheels are configurated for minimized the electric power consumption. Wheels control torque and magnetic moment of magnetic torquer are limited.http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/1998/v15n1/OJOOBS_1998_v15n1_245.pdf |
| spellingShingle | Ju-Young Du Kyu-Hong Choi Sanguk-Lee Study on the Attitude Control of Spacecraft Using Reaction Wheels Journal of Astronomy and Space Sciences |
| title | Study on the Attitude Control of Spacecraft Using Reaction Wheels |
| title_full | Study on the Attitude Control of Spacecraft Using Reaction Wheels |
| title_fullStr | Study on the Attitude Control of Spacecraft Using Reaction Wheels |
| title_full_unstemmed | Study on the Attitude Control of Spacecraft Using Reaction Wheels |
| title_short | Study on the Attitude Control of Spacecraft Using Reaction Wheels |
| title_sort | study on the attitude control of spacecraft using reaction wheels |
| url | http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/1998/v15n1/OJOOBS_1998_v15n1_245.pdf |
| work_keys_str_mv | AT juyoungdu studyontheattitudecontrolofspacecraftusingreactionwheels AT kyuhongchoi studyontheattitudecontrolofspacecraftusingreactionwheels AT sanguklee studyontheattitudecontrolofspacecraftusingreactionwheels |