Abstract
This study presents a design procedure for a new robust nonlinear control algorithm based on the theory of the terminal sliding mode (TSM) to control the attitude of a satellite system. Since the traditional TSM controllers include a discontinuous function, a significant problem called chattering can occur. In this paper, a methodology for designing a new switching function is discussed to alleviate this drawback over time. Besides, to highlight the robustness of the proposed method against uncertainties, a satellite with three pairs of thrusters subject to parameter variation is simulated.
| Original language | English |
|---|---|
| Title of host publication | Advances In The Astronautical Sciences |
| Publisher | Univelt Inc. |
| Pages | 3533-3541 |
| Number of pages | 9 |
| Volume | 152 |
| ISBN (Electronic) | 9780877036111 |
| Publication status | Published - 2014 |
| Event | 24th AAS/AIAA Space Flight Mechanics Meeting, 2014 - Mexico, United States Duration: Jan 26 2014 → Jan 30 2014 |
Other
| Other | 24th AAS/AIAA Space Flight Mechanics Meeting, 2014 |
|---|---|
| Country/Territory | United States |
| City | Mexico |
| Period | 1/26/14 → 1/30/14 |
All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Space and Planetary Science