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This paper presents a new approach with a fuzzified eigensystem realization algorithm for identification of flight vehicle models in low-speed wind tunnel (LSWT) and high-speed wind tunnel (HSWT). A variety of variables in model types and testing environment (such as angle-of-attack, sideslip angle, tunnel wind speed) and profile, elevator, and power system (motor and propeller) of mini unmanned aerial...
A novel fuzzy logic-based missile terminal guidance law is proposed based on the specific feature of the fuzzy logic system. The guidance is partitioned into three stages in accordance with the relative range between the interceptor and target. Estimated line-of-sight (LOS) angle, LOS angle rate, LOS angular acceleration and relative range are used to constitute the rule antecedent of the guidance...
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