首页> 外国专利> ARTIFICIAL INTELLIGENCE NAVIGATION GUIDE CONTROLLER OF SPACE AIRFRAME

ARTIFICIAL INTELLIGENCE NAVIGATION GUIDE CONTROLLER OF SPACE AIRFRAME

机译:空间飞机的人工智能导航导航控制器

摘要

PURPOSE:To reduce a wt., a volume and power consumption and to increase the tolerance to space radiation by temporarily storing the data read by a reading control mechanism in a memory buffer in a form utilized in an inference mechanism. CONSTITUTION:A navigation guide controller 1 receives the navigation guide control signal from a navigation guide control sensor 7 and navigation guide control operation is performed in an on-board calculated 2 by artificial intelligence and an actuator 8 is driven to perform the guide control of a space airframe. Artificial intelligence operation is performed by the action of the inference mechanism 3 mounted in the calculator. The part gathering name of the intelligence base used in the calculator 2 is allowed to communicate with the reading control mechanism 5 of the intelligence base from the inference mechanism 3. The part concerned in the intelligence base stored in a CD.ROM 6 is read to be temporarily stored in the memory buffer in a main memory. The operation in the inference mechanism 3 is performed using the partial gathering of the intelligence base stored in the memory buffer 4.
机译:目的:为了减少重量,体积和功耗,并通过以推理机制中使用的形式将由读取控制机制读取的数据临时存储在存储缓冲区中,来增加对空间辐射的容忍度。组成:导航控制器1接收来自导航传感器7的导航信号,并在由人工智能计算出的车载2中进行导航控制操作,并驱动致动器8对导航仪进行导航控制。太空机身。人工智能操作通过安装在计算器中的推理机构3的作用来执行。允许计算器2中使用的情报库的部分集合名称与来自推理机构3的情报库的读取控制机构5进行通信。将与存储在CD.ROM 6中的情报库有关的部分读入。暂时存储在主存储器的存储缓冲区中。使用存储在存储缓冲器4中的智能库的部分收集来执行推理机制3中的操作。

著录项

  • 公开/公告号JPH0287011A

    专利类型

  • 公开/公告日1990-03-27

    原文格式PDF

  • 申请/专利权人 NEC CORP;

    申请/专利号JP19880239123

  • 发明设计人 AOYAMA JUNICHI;

    申请日1988-09-22

  • 分类号G01C21/24;B64G1/24;

  • 国家 JP

  • 入库时间 2022-08-22 06:21:10

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