Abstract
Based on passive theory, a direct adaptive attitude control scheme for spacecraft is proposed, which can estimate unknown inertia matrix and solve the attitude control problem effectively. Theoretical analysis demonstrates that the closed control system is asymptotically stable, and a numerical simulation illustrates the effect of the proposed scheme.
| Original language | English |
|---|---|
| Pages (from-to) | 1-7 |
| Number of pages | 7 |
| Journal | Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology |
| Volume | 43 |
| Issue number | 5 |
| State | Published - May 2011 |
Keywords
- Adaptive control
- Attitude control
- Passive
- Spacecraft
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