Accession Number:

AD0843151

Title:

Sun Tracker Evaluation Tests of the Centaur Attitude Control System.

Personal Author(s):

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Report Date:

1961-11-07

Abstract:

The objective of the tests was to determine the control system stable limit cycle characteristics in each of the pitch and yaw planes, with the sun tracking system enabled. Author

Pages:

0020

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Communities Of Interest:

File Size:

0.00MB

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