Application of the Singular Perturbation Method in the Design of Real-Time Guidance Law for an Air-to-Surface Missile
碩士 === 國立成功大學 === 航空太空工程學系 === 86 === How a missile flying along the optimal trajectory which leads to a hit to a target in the minimum time is a major topic for the investigation of the design of guidance law. This is essentially a two-po...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
1998
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| Online Access: | http://ndltd.ncl.edu.tw/handle/66639207625545361372 |