Predicting, bounding and mitigating satellite attitude disturbances arising from infrared earth sensors for satellites in inclined, elliptical orbits
View Patent ↗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.
1. A system for mitigating ERGD events affecting the pitch and roll attitude of a satellite in an inclined, elliptical earth orbit which comprises a plurality of infrared earth sensors for determining satellite roll and pitch connected to means for yaw biasing said infrared earth sensors's earth scans away from ERGD areas on the earth.
2. A system for mitigating ERGD events affecting the pitch and roll of a satellite in an inclined, elliptical earth orbit which comprises a plurality of infrared earth sensors for determining satellite roll and pitch connected to means for inhibiting at least one of said infrared earth sensors' scans while said scan passes over ERGD areas on the earth.
3. A system for mitigating ERGD events affecting the pitch and roll of a satellite in an inclined, elliptical earth orbit which comprises a plurality of infrared earth sensors for determining satellite roll and pitch connected to means for using digital integrating rate assembly (DIRA) instead of said earth sensors for satellite roll and pitch determination while said scan passes over such areas.
4. A method for mitigating disturbances in roll and pitch of an earth satellite in an inclined, elliptical orbit, said disturbances arising from ERGD events in earth areas that the satellite's ES scan traverses, said satellite including infrared earth sensors for satellite roll and pitch attitude control, comprising determining where said areas are located, and mitigating the effect of said ERGD events in said areas.
5. The method of claim 4 further comprising mitigating said disturbances by yaw biasing said satellite and its ES sensors to avoid exposure of said ES sensors to said ERGO areas.
6. The method of claim 4 further comprising mitigating said ERGO disturbances by inhibiting at least one scan of said ES sensors while said satellite's ES scan traverses said areas.
7. The method of claim 4 further comprising mitigating said ERGD disturbances by ignoring ES data while said satellites scan passes over said areas, and using DIRA's for pitch and roll positioning during said passage over said areas.