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PCADGRATE
Static Version: Min --- Full Range

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

Delta/Yr below is a slope of the linear 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
ai1ax1xon0.0016.737e-04-0.05 +/- 0.28(2.12+/-15.16)e-4DEG/SIRU-1 AXIS 1X ANALOG RATENo Violation Check
off-0.0043.261e-04-3.95 +/- 0.210.00 +/- 0.00No Violation Check
ai1ax1yon0.0026.549e-04-0.05 +/- 0.270.00 +/- 0.00DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off-0.0043.247e-04-3.96 +/- 0.210.00 +/- 0.00No Violation Check
ai1ax2xon-2.160e-046.962e-04-0.07 +/- 0.29(1.11+/-18.26)e-4DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off-0.0043.244e-04-3.95 +/- 0.210.00 +/- 0.00No Violation Check
ai1ax2yon7.895e-046.708e-04-0.06 +/- 0.280.00 +/- 0.00DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off-0.0043.262e-04-3.96 +/- 0.210.00 +/- 0.00No Violation Check
ai2ax1xon0.0012.990e-04-0.05 +/- 0.200.00 +/- 0.00DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off-0.0110.002-3.75 +/- 0.15-0.01 +/- 0.04No Violation Check
ai2ax1yon0.0023.051e-04-0.05 +/- 0.200.00 +/- 0.00DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off-0.0130.002-3.76 +/- 0.150.01 +/- 0.03No Violation Check
ai2ax2xon0.0013.033e-04-0.06 +/- 0.200.00 +/- 0.00DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off-0.0110.002-3.74 +/- 0.15-(1.10+/-289.70)e-4No Violation Check
ai2ax2yon0.0023.039e-04-0.04 +/- 0.200.00 +/- 0.00DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off-0.0130.003-3.75 +/- 0.16-0.01 +/- 0.04No Violation Check
aoalpang -0.8880.023-36.83 +/- 20.140.40 +/- 0.46DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 -0.0025.171e-04-0.39 +/- 0.420.01 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 -0.0025.308e-04-0.43 +/- 0.440.01 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 -0.0024.929e-04-0.48 +/- 0.410.02 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 0.0600.044-0.18 +/- 35.800.01 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang -0.3140.020-44.09 +/- 16.970.38 +/- 0.39DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 -0.0025.174e-04-0.39 +/- 0.420.02 +/- 0.01naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 -0.0025.309e-04-0.43 +/- 0.440.01 +/- 0.01naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 -0.0024.928e-04-0.48 +/- 0.410.01 +/- 0.01naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 2.073e+0332.137-(2.05+/-3.11)e4(8.22+/-2.52)e2KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 -1.018e+044.106e+04-(3.94+/-337.10)e5(8.48+/-2.87)e2KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 1.257e+0352.998(2.77+/-4.46)e4(2.25+/-0.38)e3KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 0.0030.003-1.19 +/- 2.060.11 +/- 0.03KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 -0.0110.002-1.36 +/- 1.760.09 +/- 0.02KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 -0.0070.002-1.40 +/- 1.450.10 +/- 0.02KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 7.991e-048.815e-04-0.01 +/- 0.720.00 +/- 0.01naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 -4.124e-047.897e-04(4.26+/-6480.00)e-40.00 +/- 0.01naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 3.909e-043.404e-04-0.00 +/- 0.280.00 +/- 0.00naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 -9.275e-041.878e-05-0.02 +/- 0.020.00 +/- 0.00naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 -0.0025.971e-05-0.04 +/- 0.050.00 +/- 0.00naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 4.514e-069.672e-07-1.00 +/- 0.00(6.48+/-3.79)e-7naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 -0.0025.077e-04-0.35 +/- 0.420.01 +/- 0.01naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 -0.0025.266e-04-0.40 +/- 0.430.01 +/- 0.01naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 -0.0024.809e-04-0.45 +/- 0.400.02 +/- 0.01naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

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

Data Updated: Mar 11, 2026
Last Site Modification: Sep 30, 2021