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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 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
ai1ax1xon0.0026.438e-04-0.04 +/- 0.27(3.15+/-15.18)e-4DEG/SIRU-1 AXIS 1X ANALOG RATENo Violation Check
off-0.0054.880e-04-3.94 +/- 0.230.00 +/- 0.00No Violation Check
ai1ax1yon0.0026.239e-04-0.05 +/- 0.260.00 +/- 0.00DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off-0.0064.862e-04-3.96 +/- 0.230.00 +/- 0.00No Violation Check
ai1ax2xon1.306e-046.683e-04-0.07 +/- 0.28(2.08+/-18.30)e-4DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off-0.0054.851e-04-3.94 +/- 0.230.00 +/- 0.00No Violation Check
ai1ax2yon0.0016.411e-04-0.06 +/- 0.270.00 +/- 0.00DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off-0.0064.887e-04-3.96 +/- 0.230.00 +/- 0.00No Violation Check
ai2ax1xon0.0014.287e-04-0.06 +/- 0.220.00 +/- 0.00DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off-0.0140.003-3.75 +/- 0.15-0.01 +/- 0.04No Violation Check
ai2ax1yon0.0024.375e-04-0.05 +/- 0.220.00 +/- 0.00DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off-0.0170.003-3.76 +/- 0.150.01 +/- 0.03No Violation Check
ai2ax2xon0.0024.347e-04-0.06 +/- 0.220.00 +/- 0.00DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off-0.0130.003-3.74 +/- 0.15-(1.07+/-290.60)e-4No Violation Check
ai2ax2yon0.0024.358e-04-0.04 +/- 0.220.00 +/- 0.00DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off-0.0160.003-3.75 +/- 0.16-0.01 +/- 0.04No Violation Check
aoalpang -1.1280.029-35.83 +/- 20.390.01 +/- 0.56DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 -0.0046.455e-04-0.39 +/- 0.420.01 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 -0.0036.689e-04-0.43 +/- 0.440.01 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 -0.0046.053e-04-0.49 +/- 0.400.03 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 0.0750.060-0.25 +/- 39.200.01 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang -0.4460.026-43.91 +/- 17.340.16 +/- 0.48DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 -0.0046.459e-04-0.39 +/- 0.420.01 +/- 0.01naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 -0.0036.690e-04-0.43 +/- 0.440.01 +/- 0.01naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 -0.0046.055e-04-0.49 +/- 0.400.02 +/- 0.01naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 2.603e+0339.950-(2.30+/-3.18)e4(9.42+/-2.41)e2KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 -3.134e+045.635e+04-(4.51+/-369.20)e5-6.73 +/- 294.98KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 1.312e+0368.369(2.52+/-4.57)e4(1.55+/-0.39)e3KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 0.0440.002-1.04 +/- 1.540.04 +/- 0.02KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 -0.0240.003-1.38 +/- 1.760.05 +/- 0.02KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 -0.0400.002-1.51 +/- 1.480.09 +/- 0.02KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 -1.344e-040.001-0.02 +/- 0.73-0.01 +/- 0.01naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 0.0039.863e-040.01 +/- 0.650.00 +/- 0.01naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 0.0024.244e-04(7.64+/-2780.00)e-40.00 +/- 0.00naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 -8.018e-042.143e-05-0.02 +/- 0.01(6.84+/-4.01)e-4naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 -0.0027.075e-05-0.03 +/- 0.05-(3.73+/-13.49)e-4naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 5.453e-061.150e-06-1.00 +/- 0.00(0.00+/-0.00)e0naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 -0.0046.340e-04-0.36 +/- 0.420.01 +/- 0.01naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 -0.0036.647e-04-0.40 +/- 0.440.01 +/- 0.01naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 -0.0045.920e-04-0.45 +/- 0.390.02 +/- 0.01naTARGET 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