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Iterative Learning Control for homing guidance design of missiles 被引量:2
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作者 leonardo acho 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2017年第5期360-366,共7页
This paper presents an Iterative Learning Control design applied to homing guidance of missiles against maneuvering targets. According to numerical experiments, although an increase of the control energies is apprecia... This paper presents an Iterative Learning Control design applied to homing guidance of missiles against maneuvering targets. According to numerical experiments, although an increase of the control energies is appreciated with respect to a previous published base controller for comparison, this strategy, which is simple to realize, is able to reduce the time to reach the head-on condition to target destruction. This fact is important to minimize the missile lateral force-level to fulfill engaging in hyper-sonic target persecutions. 展开更多
关键词 TERMINAL GUIDANCE LAW Missiles ITERATIVE LEARNING control
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