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Title:
ROCKET CONTROL DEVICE
Document Type and Number:
Japanese Patent JPH0310997
Kind Code:
A
Abstract:

PURPOSE: To enable free time control with various conditions by providing a memory circuit saving several patterns of a launching sequence at the time of launching a rocket, and a sequence pattern selector circuit.

CONSTITUTION: A memory circuit 21 storing several patterns of a launching sequence at the time of launching a rocket is provided, and a time generation part 25 is also provided for generating reference time for outputting each sequence pattern. In addition, the memory circuit 21 is connected to a selector control circuit 22 inputted with a select signal from an external signal input circuit 24. When a rocket or a flying body is launched, the sequence of the memory circuit 21-1 is used to control the flying body. Also, when an external activation signal is received with an altimeter, a ground command or the like, the sequence of the memory circuit 21-2 is used to control the flying body. Furthermore, when the flying body lands on a sea surface, the sequence of the memory circuit 21-3 is used to control the flying body.


Inventors:
KIKUCHI TAKESHI
Application Number:
JP14543689A
Publication Date:
January 18, 1991
Filing Date:
June 09, 1989
Export Citation:
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Assignee:
MATSUSHITA ELECTRIC IND CO LTD
International Classes:
B64G1/00; B64G1/14; B64G1/24; F41G7/34; G05D1/10; F41G7/00; (IPC1-7): B64G1/00; B64G1/24; F41G7/00; F41G7/34; G05D1/10
Attorney, Agent or Firm:
Koji Hoshino



 
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