Computer Science – Performance
Scientific paper
Feb 1993
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1993fmet.symp...55m&link_type=abstract
In its Flight Mechanics/Estimation Theory Symposium, 1992 p 55-68 (SEE N93-24694 09-13)
Computer Science
Performance
Angular Momentum, Attitude Indicators, Boresights, Heavy Ions, Kalman Filters, Onboard Equipment, Pulse Duration Modulation, Reaction Wheels, Satellite Attitude Control, Satellite Instruments, Solar Sensors, Telescopes, Algorithms, Equinoxes, Feedback Control, Performance Tests, Simulators, Solstices, Vax Computers, Winter
Scientific paper
Algorithms for on-board attitude determination and control of the Solar, Anomalous, and Magnetospheric Particle Explorer (SAMPEX) have been expanded to include a constant gain Kalman filter for the spacecraft angular momentum, pulse width modulation for the reaction wheel command, an algorithm to avoid pointing the Heavy Ion Large Telescope (HILT) instrument boresight along the spacecraft velocity vector, and the addition of digital sun sensor (DSS) failure detection logic. These improved algorithms were tested in a closed-loop environment for three orbit geometries, one with the sun perpendicular to the orbit plane, and two with the sun near the orbit plane - at Autumnal Equinox and at Winter Solstice. The closed-loop simulator was enhanced and used as a truth model for the control systems' performance evaluation and sensor/actuator contingency analysis. The simulations were performed on a VAX 8830 using a prototype version of the on-board software.
Flatley Thomas W.
Henretty Debra A.
Markley Landis F.
McCullough Jon D.
San Josephine K.
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