Title:
ARTIFICIAL INTELLIGENCE NAVIGATION GUIDE CONTROLLER OF SPACE AIRFRAME
Document Type and Number:
Japanese Patent JPH0287011
Kind Code:
A
Abstract:
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.
Inventors:
AOYAMA JUNICHI
Application Number:
JP23912388A
Publication Date:
March 27, 1990
Filing Date:
September 22, 1988
Export Citation:
Assignee:
NEC CORP
International Classes:
G01C21/24; B64G1/24; (IPC1-7): B64G1/24; G01C21/24
Attorney, Agent or Firm:
Ozeki Shinsuke
Next Patent: JPH0287012