運用奇異線性指數二次高斯及迴路轉移函數回歸法從事傾斜轉彎自動駕儀之設計研究
碩士 === 國防大學中正理工學院 === 電子工程研究所 === 91 === In this thesis, a bank-to-turn missile autopilot is designed by using the Generalized Singular Linear Exponential Quadratic Gaussian and Loop Transfer Recovery techniques. The Generalized Singular Linear Exponential Quadratic Gaussian method is adopted for tw...
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2004
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| Online Access: | http://ndltd.ncl.edu.tw/handle/33592240741984642557 |
| Summary: | 碩士 === 國防大學中正理工學院 === 電子工程研究所 === 91 === In this thesis, a bank-to-turn missile autopilot is designed by using the Generalized Singular Linear Exponential Quadratic Gaussian and Loop Transfer Recovery techniques. The Generalized Singular Linear Exponential Quadratic Gaussian method is adopted for two reasons. The first reason is that the process noise and measurement noise are considered in the system design so the robustness of the system is preserved. The second reason is this method can overcome the limitation in controller design of the Generalized Singular Linear Quadratic technique.
Finally, numerical simulation results show that the Roll-Pitch-Yaw aerodynamic cross-coupling problems are solved and the stability of the system is also enhanced.
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