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Star tracker operation in a high density proton fieldAlgorithms that reject transient signals due to proton effects on charge coupled device (CCD) sensors have been implemented in the HDOS ASTRA-l Star Trackers to be flown on the TOPEX mission scheduled for launch in July 1992. A unique technique for simulating a proton-rich environment to test trackers is described, as well as the test results obtained. Solar flares or an orbit that passes through the South Atlantic Anomaly can subject the vehicle to very high proton flux levels. There are three ways in which spurious proton generated signals can impact tracker performance: the many false signals can prevent or extend the time to acquire a star; a proton-generated signal can compromise the accuracy of the star's reported magnitude and position; and the tracked star can be lost, requiring reacquisition. Tests simulating a proton-rich environment were performed on two ASTRA-1 Star Trackers utilizing these new algorithms. There were no false acquisitions, no lost stars, and a significant reduction in reported position errors due to these improvements.
Document ID
19930015510
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Miklus, Kenneth J.
(Hughes Danbury Optical Systems Inc., CT, United States)
Kissh, Frank
(Hughes Danbury Optical Systems Inc., CT, United States)
Flynn, David J.
(Hughes Danbury Optical Systems Inc., CT, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1993
Publication Information
Publication: NASA. Goddard Space Flight Center, Flight Mechanics(Estimation Theory Symposium, 1992
Subject Category
Spacecraft Instrumentation
Accession Number
93N24699
Funding Number(s)
CONTRACT_GRANT: JPL-957849
Distribution Limits
Public
Copyright
Public Use Permitted.
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