发明名称 Neural network controller for a pulsed rocket motor tactical missile system
摘要 A neural network controller for a pulsed rocket motor tactical missile. The missile includes a fuselage or body, with a propulsion system. The pulsed propulsion system has a need for a logical control of the application of propulsion energy throughout the missile's flight. The controller is trained to provide optimal initiation of individual rocket motor thrust pulses based on tactical information available at various points/times in the missile's flight. The controller training is through use of training cases, in which the network learns to output a specific target value(s) when specific values are input. When trained with a large sample of training cases selected from the multidimensional population of interest, the neural network effectively learns the correlations between inputs and outputs and can predict input/output relationships not previously seen in any training case.
申请公布号 AU6237199(A) 申请公布日期 2000.01.05
申请号 AU19990062371 申请日期 1999.01.06
申请人 RAYTHEON COMPANY 发明人 JAMES E. BIGGERS;KEVIN P. FINN;HOMER H. SCHWARTZ II
分类号 F42B10/38;F42B10/66;F42B15/00 主分类号 F42B10/38
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