ATTITUDE CONTROL DEVICE FOR SPACE VEHICLE

PROBLEM TO BE SOLVED: To enhance accuracy in attitude stability and prolong life. SOLUTION: First to fourth driving wheels 12-15 are rotatably mounted on a space vehicle 10, and the first to fourth driving wheels 12-15 are driven and controlled in a sated that the number of revolutions is offset and...

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Bibliographic Details
Main Author YOSHIZAWA TAKESHI
Format Patent
LanguageEnglish
Published 22.05.2002
Edition7
Subjects
AIRCRAFT
AVIATION
COSMONAUTICS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
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Summary:PROBLEM TO BE SOLVED: To enhance accuracy in attitude stability and prolong life. SOLUTION: First to fourth driving wheels 12-15 are rotatably mounted on a space vehicle 10, and the first to fourth driving wheels 12-15 are driven and controlled in a sated that the number of revolutions is offset and so that the summation of angular momentum is kept in the vicinity of 0, to control the attitude of the space vehicle 10.
Bibliography:Application Number: JP20000345585