Title:
FLYING GUIDANCE CONTROLLER FOR SPACE MACHINE
Document Type and Number:
Japanese Patent JPH06138944
Kind Code:
A
Abstract:
PURPOSE: To mount a highly accurate and safe guidance controller on a space machine and to secure the highly accurate and safe flying guidance control of the space machine by attaining the decentralized processing by means of the computers of the same calculation algorithm.
CONSTITUTION: A guidance control rule has a linear mapping 13 of a fuzzy rule produced from the empirical rules and a non-linear mapping 14 of the input/output relation and is expressed in a common fuzzy operational expression. Then the navigation signal sent from a navigation system 1 is substituted for the fuzzy operational expression so that a control signal is obtained.
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Inventors:
YOSHIKAWA SHOJI
Application Number:
JP31113292A
Publication Date:
May 20, 1994
Filing Date:
October 28, 1992
Export Citation:
Assignee:
MITSUBISHI ELECTRIC CORP
International Classes:
G05D1/08; G05D1/10; B64G1/24; (IPC1-7): G05D1/08; B64G1/24; G05D1/10
Attorney, Agent or Firm:
Hiroaki Tazawa (2 outside)