NMPC-Based Autopilot Design for Air-to-Air Missiles
In this paper, an overload autopilot based on generalized extended state observer, predictive function control and improved barrier interior-point method is designed to solve the problems of model nonlinearity, time variability and control constraints in attitude control of air-to-air missile. First...
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| Auteur principal: | |
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| Format: | article |
| Langue: | ZH |
| Publié: |
Editorial Office of Aero Weaponry
2021
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| Accès en ligne: | https://doaj.org/article/3b50e01c447f4979aec100389195ec10 |
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