Application of Gain Scheduling and Fuzzy Control in Missile Guidance and Control System esign
碩士 === 逢甲大學 === 自動控制工程學系 === 87 === Actual aerodynamically controlled missiles are nonlinear: their dynamics changes with the operating points and may be essential nonlinearities in the plant. For the sack of simplification in designs, traditional aerodynamically controlled missiles are usually guid...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
1999
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| Online Access: | http://ndltd.ncl.edu.tw/handle/72561600792637564124 |