Predicting, bounding and mitigating satellite attitude disturbances arising from infrared earth sensors for satellites in inclined, elliptical orbits

Satellite earth sensors (ES) generate scan lines, areas of detected infrared information gathered across the view of the earth by the satellite. The length of these scan lines is utilized by the satellite Attitude Control Subsystem (ACS) to determine the satellite pointing in roll and pitch. There a...

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Hauptverfasser: HESSLER, III THEODORE, ANGLIN PATRICK T, CROOM CHRISTOPHER A, BOUNDS RONALD W, KOKKALAKIS MICHAEL, LAM CLAUDIA H, CRAWFORD PAUL W
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creator HESSLER, III THEODORE
ANGLIN PATRICK T
CROOM CHRISTOPHER A
BOUNDS RONALD W
KOKKALAKIS MICHAEL
LAM CLAUDIA H
CRAWFORD PAUL W
description Satellite earth sensors (ES) generate scan lines, areas of detected infrared information gathered across the view of the earth by the satellite. The length of these scan lines is utilized by the satellite Attitude Control Subsystem (ACS) to determine the satellite pointing in roll and pitch. There are areas on the earth during particular periods of the year that can cause earth radiance gradient disturbance effects, satellite attitude errors caused by the ACS-calculated length of the scan lines becoming faulted. This invention includes methods and systems for minimizing disturbances to the satellite attitude for satellites in inclined, elliptical orbits that use infrared earth sensors to determine pitch and roll angles. These include identifying areas where earth radiance gradient events cause such disturbances and the prediction of times of such occurrences and methods for mitigating the effect of such events.
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subjects AIRCRAFT
ANALOGOUS ARRANGEMENTS USING OTHER WAVES
AVIATION
COSMONAUTICS
DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES
LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES
MEASURING
PERFORMING OPERATIONS
PHYSICS
RADIO DIRECTION-FINDING
RADIO NAVIGATION
TESTING
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
title Predicting, bounding and mitigating satellite attitude disturbances arising from infrared earth sensors for satellites in inclined, elliptical orbits
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