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|Title:||Missile guidance algorithm design using inverse kinematics and fuzzy logic|
Guidance algorithm design
|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|
|Appears in Collections:||Staff Publications|
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