Abstract
The problem of missile interception is investigated in this paper. Sliding-mode controllers with finite-time convergence are proposed for the design of guidance laws. In particular, the control design consists of the estimation of the target acceleration by the extended state observer (ESO), and thus, it achieves the decrease of undesired chattering effectively. Also, simulation results are presented to illustrate the effectiveness of the control strategies.
| Original language | English |
|---|---|
| Article number | 6374675 |
| Pages (from-to) | 5882-5891 |
| Number of pages | 10 |
| Journal | IEEE Transactions on Industrial Electronics |
| Volume | 60 |
| Issue number | 12 |
| DOIs | |
| Publication status | Published - 2013 |
Keywords
- Extended state observer (ESO)
- finite-time control
- guidance law
- sliding-mode control (SMC)
Fingerprint
Dive into the research topics of 'Missile guidance law based on extended state observer'. Together they form a unique fingerprint.Cite this
Zhu, Z., Xu, D., Liu, J., & Xia, Y. (2013). Missile guidance law based on extended state observer. IEEE Transactions on Industrial Electronics, 60(12), 5882-5891. Article 6374675. https://doi.org/10.1109/TIE.2012.2232254