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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-6.477e-043.578e-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-0.0023.591e-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-0.0013.602e-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-0.0023.593e-04-3.80 +/- 0.24-0.01 +/- 0.00No Violation Check
ai2ax1xon0.0011.989e-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
ai2ax1yon6.357e-042.003e-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
ai2ax2xon8.988e-042.002e-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
ai2ax2yon8.874e-041.992e-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 0.3550.02223.54 +/- 19.07-1.31 +/- 0.41DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 0.6100.5254.68 +/- 445.79-0.01 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 0.0025.171e-040.40 +/- 0.44-0.00 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 -1.2660.8997.68 +/- 762.92-0.02 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 0.0030.0020.66 +/- 1.43-0.00 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang 0.2290.02939.14 +/- 24.92-1.56 +/- 0.60DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 -4.131e+066.178e+06(5.10+/-524.30)e7-0.02 +/- 0.01naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 0.0025.176e-040.40 +/- 0.44-0.00 +/- 0.01naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 -3.474e+041.935e+04(1.56+/-164.30)e5-0.02 +/- 0.01naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 361.42631.733(2.31+/-2.71)e4-(9.53+/-2.22)e2KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 -2.280e+0358.178-(4.75+/-52.70)e3-(2.96+/-0.48)e3KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 6.47733.081(9.56+/-2.81)e4-(1.09+/-0.22)e3KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 -0.0230.0020.92 +/- 1.48-0.02 +/- 0.01KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 -0.0350.0021.39 +/- 1.70-0.12 +/- 0.02KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 -0.0230.0021.43 +/- 1.52-0.08 +/- 0.02KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 7.160e-048.340e-04(1.67+/-7080.00)e-4-0.02 +/- 0.01naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 0.0027.626e-040.03 +/- 0.650.01 +/- 0.01naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 3.082e-043.365e-040.01 +/- 0.290.00 +/- 0.00naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 6.133e-051.148e-040.01 +/- 0.10-(7.41+/-2.18)e-4naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 0.0025.183e-050.04 +/- 0.05-0.00 +/- 0.00naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 -8.538e-069.739e-05-0.99 +/- 0.08-(2.96+/-1.81)e-4naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 0.0024.755e-040.39 +/- 0.40-0.01 +/- 0.01naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 0.0025.105e-040.36 +/- 0.43-0.01 +/- 0.01naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 0.0014.911e-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: Oct 03, 2026
Last Site Modification: Sep 30, 2021