제어로봇시스템학회:학술대회논문집
- 1993.10a
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- Pages.1063-1067
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- 1993
Design of missile roll controller based on the fuzzy logic
퍼지논리를 이용한 유도탄 롤 제어기 설계
Abstract
Fuzzy logic is applied to a roll autopilot for missiles. Fuzzy rules are made so that the response duplicates that of the conventional control law for some flight condition. A scaling factor of the fuzzy controller is then scheduled by the missile velocity and altitude information to cope with the variation of the roll dynamics from that flight condition. By computer simulations and calculation of the stability margin, it is shown that the fuzzy control is robuster than the conventional one over the flight envelope even though two control laws work similarly for some flight conditions.
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