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PCADGRATE
Static Version: Max --- 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
ai1ax1xon-0.0023.745e-040.01 +/- 0.16(6.18+/-9.60)e-4DEG/SIRU-1 AXIS 1X ANALOG RATENo Violation Check
off-6.492e-043.586e-04-3.77 +/- 0.24-0.01 +/- 0.00No Violation Check
ai1ax1yon-0.0033.750e-040.01 +/- 0.16-(5.97+/-11.45)e-4DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off-0.0023.598e-04-3.81 +/- 0.24-0.01 +/- 0.00No Violation Check
ai1ax2xon3.606e-043.558e-040.04 +/- 0.15-(6.76+/-14.08)e-4DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off-0.0013.610e-04-3.79 +/- 0.24-0.01 +/- 0.00No Violation Check
ai1ax2yon-7.495e-043.619e-040.03 +/- 0.15-(5.99+/-12.92)e-4DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off-0.0023.600e-04-3.80 +/- 0.24-0.01 +/- 0.00No Violation Check
ai2ax1xon0.0011.992e-040.03 +/- 0.14-0.00 +/- 0.00DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off0.0080.005-3.69 +/- 0.300.01 +/- 0.00No Violation Check
ai2ax1yon6.364e-042.007e-040.03 +/- 0.14-0.00 +/- 0.00DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off0.0020.005-3.69 +/- 0.340.00 +/- 0.02No Violation Check
ai2ax2xon8.959e-042.006e-040.03 +/- 0.14-0.00 +/- 0.00DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off0.0050.005-3.69 +/- 0.300.01 +/- 0.01No Violation Check
ai2ax2yon8.880e-041.996e-040.02 +/- 0.14-0.00 +/- 0.00DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off0.0020.005-3.69 +/- 0.320.01 +/- 0.02No Violation Check
aoalpang 0.3560.02223.54 +/- 19.08-1.31 +/- 0.41DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 0.6120.5264.68 +/- 446.01-0.01 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 0.0025.179e-040.40 +/- 0.44-0.00 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 -1.2680.9007.69 +/- 763.30-0.02 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 0.0030.0020.66 +/- 1.43-(1.70+/-59.19)e-4naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang 0.2300.02939.14 +/- 24.92-1.58 +/- 0.60DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 -4.131e+066.189e+06(5.10+/-524.60)e7-0.02 +/- 0.01naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 0.0025.184e-040.40 +/- 0.44-(9.66+/-103.50)e-4naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 -3.479e+041.939e+04(1.56+/-164.40)e5-0.02 +/- 0.01naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 366.50631.759(2.32+/-2.71)e4-(9.49+/-2.22)e2KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 -2.277e+0358.250-(4.71+/-52.69)e3-(2.95+/-0.48)e3KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 8.82133.122(9.56+/-2.81)e4-(1.10+/-0.22)e3KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 -0.0230.0020.93 +/- 1.48-0.02 +/- 0.01KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 -0.0350.0021.39 +/- 1.69-0.12 +/- 0.02KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 -0.0230.0021.43 +/- 1.51-0.08 +/- 0.02KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 9.097e-048.346e-040.00 +/- 0.71-0.02 +/- 0.01naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 0.0027.639e-040.03 +/- 0.650.01 +/- 0.01naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 3.142e-043.370e-040.01 +/- 0.290.00 +/- 0.00naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 6.114e-051.150e-040.01 +/- 0.10-(7.08+/-2.18)e-4naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 0.0025.185e-050.04 +/- 0.05-0.00 +/- 0.00naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 -9.555e-069.755e-05-0.99 +/- 0.08-(3.44+/-1.80)e-4naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 0.0024.759e-040.39 +/- 0.40-0.01 +/- 0.01naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 0.0025.112e-040.36 +/- 0.43-0.01 +/- 0.01naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 0.0014.917e-040.38 +/- 0.42-0.01 +/- 0.01naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

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

Data Updated: Sep 23, 2026
Last Site Modification: Sep 30, 2021