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PCADGRATE
Static Version: Min --- One Week

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
ai1ax1xon0.0050.105-0.96 +/- 1.60(1.86+/-1.94)e2DEG/SIRU-1 AXIS 1X ANALOG RATENo Violation Check
off-5.238e-042.023e-04-3.90 +/- 0.020.46 +/- 1.21No Violation Check
ai1ax1yon0.0150.106-0.96 +/- 1.62(2.04+/-1.97)e2DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off-3.860e-059.892e-05-3.94 +/- 0.010.42 +/- 0.53No Violation Check
ai1ax2xon0.0010.106-0.94 +/- 1.62(1.93+/-1.97)e2DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off-2.096e-041.286e-04-3.91 +/- 0.010.16 +/- 0.68No Violation Check
ai1ax2yon0.0150.106-0.96 +/- 1.62(2.00+/-1.97)e2DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off-2.342e-059.177e-05-3.94 +/- 0.01-0.14 +/- 0.45No Violation Check
ai2ax1xon1.700e-041.329e-04-0.00 +/- 0.01-0.13 +/- 1.29DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off-2.4320.064-1.53 +/- 1.79-50.59 +/- 87.65No Violation Check
ai2ax1yon3.841e-041.373e-04-0.00 +/- 0.011.86 +/- 1.27DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off-2.5350.066-1.56 +/- 1.86-58.68 +/- 90.54No Violation Check
ai2ax2xon3.309e-051.414e-04-0.01 +/- 0.011.90 +/- 1.29DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off-2.5160.066-1.55 +/- 1.85-55.90 +/- 89.76No Violation Check
ai2ax2yon2.685e-049.420e-05-(8.80+/-90.00)e-40.85 +/- 0.77DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off-2.5200.066-1.56 +/- 1.85-59.77 +/- 90.71No Violation Check
aoalpang 0.1420.235-11.77 +/- 21.23-42.84 +/- 2104.18DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 -0.1270.0050.24 +/- 0.53-26.21 +/- 19.13naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 0.0880.0030.32 +/- 0.3624.80 +/- 21.93naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 -0.0730.004-0.01 +/- 0.35-23.49 +/- 21.83naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 0.0200.0020.50 +/- 0.223.51 +/- 17.17naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang 1.9250.301-17.36 +/- 27.49-(2.68+/-2.58)e3DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 -0.1270.0050.24 +/- 0.53-26.09 +/- 19.13naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 0.0880.0030.32 +/- 0.3624.89 +/- 21.92naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 -0.0730.004-0.01 +/- 0.35-23.43 +/- 21.83naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 1.151e+03256.265-(1.15+/-2.28)e4-(1.93+/-29.40)e4KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 -824.733439.016-(7.62+/-3.89)e4(7.53+/-6.24)e5KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 -1.117e+03391.737(6.51+/-3.47)e4-(6.77+/-5.53)e5KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 0.0070.0090.10 +/- 0.824.74 +/- 20.84KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 0.0300.015-0.09 +/- 1.370.45 +/- 24.14KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 -0.0290.014-0.10 +/- 1.22-12.94 +/- 21.94KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 -0.0083.266e-05-0.90 +/- 0.010.06 +/- 0.07naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 -0.0143.212e-050.41 +/- 0.030.07 +/- 0.16naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 -0.0063.369e-050.17 +/- 0.010.00 +/- 0.05naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 -8.740e-049.140e-05-0.00 +/- 0.01-2.29 +/- 0.67naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 -4.021e-042.317e-04(6.11+/-210.00)e-43.42 +/- 1.00naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 5.174e-051.006e-05-1.00 +/- 0.000.01 +/- 0.01naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 -0.1280.0050.25 +/- 0.52-18.97 +/- 19.89naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 0.0860.0040.32 +/- 0.3723.94 +/- 22.68naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 -0.0740.004-0.00 +/- 0.35-9.26 +/- 22.59naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

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

Data Updated: Sep 01, 2026
Last Site Modification: Sep 30, 2021