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PCADGRATE
Static Version: Max --- Last Three Months

One Week Three Month One Year Five Year Full Range Min Mean Max

Delta/Yr below is a slope of the liear fitting over the data of the period. Delta/Yr/Yr is a slope of the liner fitting over the devivative data of the period. Slope listed on a linked plot is the slope computed on the last few periods of the data to show the direction of the trend, and different from that of Delta/Yr.

MSID MeanRMSDelta/YrDelta/Yr/YrUnitDescriptionLimit Violation
ai1ax1xon-0.0030.004-0.06 +/- 0.01(0.00+/-0.00)e0DEG/SIRU-1 AXIS 1X ANALOG RATENo Violation Check
off2.983e-048.397e-05-3.83 +/- 0.190.01 +/- 0.00No Violation Check
ai1ax1yon3.796e-14999.000-0.06 +/- 0.00(0.00+/-0.00)e0DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off3.161e-048.448e-05-3.87 +/- 0.190.01 +/- 0.00No Violation Check
ai1ax2xon3.796e-14999.000-0.06 +/- 0.00(0.00+/-0.00)e0DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off3.114e-048.463e-05-3.86 +/- 0.190.00 +/- 0.00No Violation Check
ai1ax2yon-0.0030.004-0.06 +/- 0.01(0.00+/-0.00)e0DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off3.172e-048.446e-05-3.86 +/- 0.190.01 +/- 0.00No Violation Check
ai2ax1xon7.357e-066.580e-060.01 +/- 0.01(4.51+/-15.78)e-4DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off-1.2810.504-3.45 +/- 0.97(0.00+/-0.00)e0No Violation Check
ai2ax1yon-3.066e-057.780e-060.00 +/- 0.020.01 +/- 0.00DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off-0.0400.033-3.86 +/- 0.05(0.00+/-0.00)e0No Violation Check
ai2ax2xon-1.021e-058.886e-060.00 +/- 0.020.00 +/- 0.00DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off-0.0420.034-3.82 +/- 0.05(0.00+/-0.00)e0No Violation Check
ai2ax2yon-1.685e-055.921e-060.00 +/- 0.010.00 +/- 0.00DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off-0.0500.039-3.86 +/- 0.06(0.00+/-0.00)e0No Violation Check
aoalpang -0.0180.011-9.06 +/- 25.574.83 +/- 3.91DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 -0.0031.924e-040.02 +/- 0.450.02 +/- 0.12naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 3.150e-041.738e-040.41 +/- 0.39-0.07 +/- 0.06naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 0.0021.702e-04-0.07 +/- 0.39-0.03 +/- 0.09naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 0.0021.111e-040.57 +/- 0.27-0.04 +/- 0.06naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang 0.0350.017-2.64 +/- 38.222.48 +/- 5.47DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 -0.0031.919e-040.02 +/- 0.450.03 +/- 0.12naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 1.903e-041.751e-040.40 +/- 0.40-0.17 +/- 0.07naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 0.0021.697e-04-0.08 +/- 0.39-0.04 +/- 0.09naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 7.45410.355(1.46+/-2.33)e4(6.10+/-111.36)e2KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 5.65017.204-(8.39+/-3.88)e4-(4.30+/-18.76)e3KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 7.50511.679(6.38+/-2.63)e4(2.17+/-12.73)e3KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 7.674e-053.173e-040.10 +/- 0.71-0.02 +/- 0.23KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 4.853e-046.388e-040.16 +/- 1.440.14 +/- 0.49KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 -2.922e-044.610e-040.07 +/- 1.04-0.08 +/- 0.36KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 -0.0067.295e-05-0.72 +/- 0.290.09 +/- 0.01naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 -0.0125.242e-050.31 +/- 0.49-0.03 +/- 0.01naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 -0.0052.276e-050.14 +/- 0.21-0.01 +/- 0.00naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 2.138e-053.353e-06-0.00 +/- 0.01-(2.95+/-93.28)e-5naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 -2.885e-051.625e-050.01 +/- 0.040.01 +/- 0.01naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 3.505e-051.341e-05-1.00 +/- 0.03(5.51+/-6.59)e-4naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 -0.0031.909e-040.01 +/- 0.450.02 +/- 0.12naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 3.341e-041.757e-040.40 +/- 0.40-0.14 +/- 0.07naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 0.0021.697e-04-0.08 +/- 0.39-0.07 +/- 0.09naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

If you have any questions, please contact swolk@cfa.harvard.edu.

Data Updated: Nov 10, 2022
Last Site Modification: Sep 30, 2021