Missile guidance algorithm design using inverse kinematics and fuzzy logic
Fuzzy Sets and Systems
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sg-nus-scholar.10635-584882015-01-28T20:31:25Z Missile guidance algorithm design using inverse kinematics and fuzzy logic Leng, G. MECHANICAL & PRODUCTION ENGINEERING Aerospace engineering Guidance algorithm design Inverse kinematics Fuzzy Sets and Systems 79 3 287-295 FSSYD 2014-06-17T05:15:07Z 2014-06-17T05:15:07Z 1996 Article Leng, G. (1996). Missile guidance algorithm design using inverse kinematics and fuzzy logic. Fuzzy Sets and Systems 79 (3) : 287-295. ScholarBank@NUS Repository. 01650114 http://scholarbank.nus.edu.sg/handle/10635/58488 NOT_IN_WOS Scopus |
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Aerospace engineering Guidance algorithm design Inverse kinematics |
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Aerospace engineering Guidance algorithm design Inverse kinematics Leng, G. Missile guidance algorithm design using inverse kinematics and fuzzy logic |
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Fuzzy Sets and Systems |
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MECHANICAL & PRODUCTION ENGINEERING |
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MECHANICAL & PRODUCTION ENGINEERING Leng, G. |
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Leng, G. |
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Leng, G. |
title |
Missile guidance algorithm design using inverse kinematics and fuzzy logic |
title_short |
Missile guidance algorithm design using inverse kinematics and fuzzy logic |
title_full |
Missile guidance algorithm design using inverse kinematics and fuzzy logic |
title_fullStr |
Missile guidance algorithm design using inverse kinematics and fuzzy logic |
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Missile guidance algorithm design using inverse kinematics and fuzzy logic |
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missile guidance algorithm design using inverse kinematics and fuzzy logic |
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2014 |
url |
http://scholarbank.nus.edu.sg/handle/10635/58488 |
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