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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
off1.388e-041.983e-04-3.89 +/- 0.02-0.52 +/- 1.30No Violation Check
ai1ax1yon0.0150.106-0.96 +/- 1.62(2.04+/-1.97)e2DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off4.659e-051.112e-04-3.94 +/- 0.01-0.27 +/- 0.58No Violation Check
ai1ax2xon0.0010.106-0.94 +/- 1.62(1.93+/-1.97)e2DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off2.017e-041.403e-04-3.91 +/- 0.01-0.20 +/- 0.73No Violation Check
ai1ax2yon0.0150.106-0.96 +/- 1.62(2.00+/-1.97)e2DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off-5.232e-051.054e-04-3.94 +/- 0.01-0.08 +/- 0.53No Violation Check
ai2ax1xon-2.605e-041.396e-04-0.00 +/- 0.011.46 +/- 1.39DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off-2.4320.064-1.53 +/- 1.79-50.59 +/- 87.65No Violation Check
ai2ax1yon-6.718e-041.423e-04-0.00 +/- 0.010.71 +/- 1.29DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off-2.5350.066-1.56 +/- 1.86-58.68 +/- 90.54No Violation Check
ai2ax2xon-4.383e-041.561e-04-0.01 +/- 0.010.89 +/- 1.46DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off-2.5160.066-1.55 +/- 1.85-55.90 +/- 89.76No Violation Check
ai2ax2yon-3.841e-041.182e-04-0.00 +/- 0.01-0.31 +/- 0.94DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off-2.5200.066-1.56 +/- 1.85-59.77 +/- 90.71No Violation Check
aoalpang -1.3560.254-12.44 +/- 24.07-(4.24+/-1.95)e3DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 0.0090.004-0.21 +/- 0.3817.93 +/- 23.57naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 1.190e-050.004-0.10 +/- 0.4119.43 +/- 34.81naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 0.0120.0060.11 +/- 0.5783.12 +/- 37.15naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 0.0100.0030.48 +/- 0.26-24.42 +/- 14.18naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang -2.4620.302-17.26 +/- 28.86(2.59+/-22.79)e2DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 0.0090.004-0.21 +/- 0.3817.84 +/- 23.56naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 3.557e-050.004-0.10 +/- 0.4119.39 +/- 34.80naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 0.0120.0060.11 +/- 0.5691.49 +/- 37.08naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 1.301e+03250.333-(8.34+/-232.50)e2-(1.05+/-0.35)e6KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 2.444e+03426.746-(8.13+/-3.97)e4(3.15+/-0.67)e6KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 -3.275e+03368.180(5.79+/-3.46)e4-(9.04+/-5.37)e5KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 -0.0660.011-0.01 +/- 1.04-86.14 +/- 32.61KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 0.1060.0160.17 +/- 1.5147.73 +/- 30.80KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 -4.611e-040.014-0.12 +/- 1.2769.25 +/- 27.60KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 0.0173.112e-050.24 +/- 0.040.12 +/- 0.25naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 0.0042.913e-05-0.89 +/- 0.01(2.70+/-0.12)e-10naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 0.0022.807e-05-0.39 +/- 0.01-(3.56+/-0.54)e-11naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 0.0021.490e-04-0.01 +/- 0.010.04 +/- 0.88naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 -0.0116.249e-040.02 +/- 0.06-0.29 +/- 2.29naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 -0.0016.113e-05-1.00 +/- 0.01-0.07 +/- 0.09naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 0.0110.004-0.20 +/- 0.3925.48 +/- 23.36naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 0.0090.004-0.10 +/- 0.4110.06 +/- 34.53naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 0.0250.0060.11 +/- 0.5760.09 +/- 35.03naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

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

Data Updated: Jan 09, 2026
Last Site Modification: Sep 30, 2021