摘要
Since the system model uncertainties and the non-Gaussain disturbance often result in filtering precision drops of Kalman filter, a class of robust H2/H∞ multi-objective control problems in integrated navigation system is studied. System error state equation of integrated navigation system is translated into polytopic description of uncertain system, and existence condition of the controller is solved by convex optimization based on linear matrix inequality (LMI). System stability is guaranteed through Lyapunov stability theory. Perturbation is attenuated through H2 and H∞ control, system rapidity is improved through guaranteed cost control and initial stage convergence is accelerated through pole placement for the non-zero initial state. Simulation results show that the robustness, convergence and precision are better.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 102-106 |
| 页数 | 5 |
| 期刊 | Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica |
| 卷 | 29 |
| 期 | SUPPL. |
| 出版状态 | 已出版 - 5月 2008 |
指纹
探究 'Multi-objective control in integrated navigation system based on LMI' 的科研主题。它们共同构成独一无二的指纹。引用此
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver