Missile IGC Based on Improved Model Predictive Control and Sliding Mode Observer
Considering recurrent optimization process in model predictive control (MPC), the model uncertainties and disturbances terms in the missile’s guidance and control model can degrade recursive feasibility, and there are control mutation problems in common MPC algorithm. This paper presents a disturban...
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| Main Authors: | Li Ma, Jiayuan Shan, Junhui Liu, Yan Ding |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2021-01-01
|
| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2021/9680346 |
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