The in-flight calibration of the Hubble Space Telescope attitude sensors

Details The in-flight calibration of the Hubble Space Telescope attitude sensors The in-flight calibration of the Hubble Space Telescope attitude sensors

Oct 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991fmet.symp..353w&link_type=abstract

In NASA. Goddard Space Flight Center, Flight Mechanics/Estimation Theory Symposium, 1991 p 353-381 (SEE N92-14070 05-13)

Computer Science

Performance

Attitude Control, Attitude Indicators, Calibrating, Guidance Sensors, Gyroscopes, Hubble Space Telescope, Magnetometers, Star Trackers, Alignment, Astrometry, Data Reduction, Distortion, Drift Rate, Magnetic Fields, Spacecraft Control

Scientific paper

A detailed review of the in-flight calibration of the Hubble Space Telescope attitude sensors is presented. The review, which covers the period from the April 24, 1990, launch of the spacecraft until the time of this writing (June 1991), describes the calibrations required and accuracies achieved for the four principal attitude sensing systems on the spacecraft: the magnetometers, the fixed head star trackers, the gyroscopes, and the fine guidance sensors (FGS's). In contrast to the other three sensor groups, the Hubble Telecope's FGS's are unique in the precision and performance levels being attempted; spacecraft control and astrometric research at the near-milliarcsecond level are the ultimate goals. FGS calibration accuracies at the 20-milliarcsecond level have already been achieved, and plans for new data acquisitions and reductions that should substantially improve these results are in progress. A summary of the basic attributes of each of the four sensor groups with respect to its usage as an attitude measuring system is presented, followed by a discussion of the calibration items of interest for that group. The calibration items are as follows: for the magnetometers, the corrections for the spacecraft's static and time-varying magnetic fields; for the fixed-head star trackers, their relative alignments and use in performing onboard attitude updates; for the gyroscopes, their scale factors, alignments, and drift rate biases; and for the FGS's, their magnifications, optical distortions, and alignments. The discussion covers the procedures used for each calibration, as well as the order of the calibrations within the general flow of orbital verification activities. It also includes a synopsis of current plans for the eventual calibration of the FGS's to achieve their near-milliarcsecond design accuracy. The conclusions include a table indicating the current and predicted ultimate accuracies for each of the calibration items.

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