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https://scholarbank.nus.edu.sg/handle/10635/58488
Title: | Missile guidance algorithm design using inverse kinematics and fuzzy logic | Authors: | Leng, G. | Keywords: | Aerospace engineering Guidance algorithm design Inverse kinematics |
Issue Date: | 1996 | Citation: | Leng, G. (1996). Missile guidance algorithm design using inverse kinematics and fuzzy logic. Fuzzy Sets and Systems 79 (3) : 287-295. ScholarBank@NUS Repository. | Abstract: | This is a feasibility study of using fuzzy logic to guide an air-to-surface missile against a stationary target. The guidance algorithm design specifications are (1) a smooth transition at lock-on, (2) inherent acceleration command limits and (3) large impact angles. Inverse kinematics is used to design the fuzzy guidance algorithm so that all three requirements are satisfied. A comparison with proportional navigation (PN) guidance is made with respect to impact angle, intercept time and command limits. It is shown that, unlike PN guidance, the combined inverse kinematics/fuzzy logic guidance scheme is able to satisfy the conflicting design requirements. © 1996 - Elsevier Science B.V. All rights reserved. | Source Title: | Fuzzy Sets and Systems | URI: | http://scholarbank.nus.edu.sg/handle/10635/58488 | ISSN: | 01650114 |
Appears in Collections: | Staff Publications |
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