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PCADGRATE
Static Version: Max --- 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
ai1ax1xon-0.0020.103-0.91 +/- 1.58(2.37+/-2.22)e2DEG/SIRU-1 AXIS 1X ANALOG RATENo Violation Check
off0.0012.638e-04-3.86 +/- 0.02-0.26 +/- 1.80No Violation Check
ai1ax1yon-0.0010.104-0.92 +/- 1.60(2.31+/-2.24)e2DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off0.0012.137e-04-3.90 +/- 0.02-0.78 +/- 1.45No Violation Check
ai1ax2xon-0.0040.104-0.92 +/- 1.60(2.35+/-2.24)e2DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off2.086e-041.431e-04-3.88 +/- 0.010.00 +/- 0.73No Violation Check
ai1ax2yon-0.0010.104-0.92 +/- 1.60(2.34+/-2.24)e2DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off3.996e-041.619e-04-3.88 +/- 0.011.05 +/- 0.83No Violation Check
ai2ax1xon-8.887e-051.568e-04(2.97+/-140.00)e-40.59 +/- 1.66DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off-2.4240.063-1.49 +/- 1.78-17.74 +/- 46.48No Violation Check
ai2ax1yon-4.702e-041.195e-04(3.17+/-100.00)e-40.03 +/- 1.17DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off-2.5140.066-1.54 +/- 1.85-26.72 +/- 47.61No Violation Check
ai2ax2xon-3.382e-041.405e-04(4.45+/-120.00)e-4-0.03 +/- 1.45DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off-2.4870.065-1.53 +/- 1.83-26.77 +/- 47.14No Violation Check
ai2ax2yon-3.140e-041.103e-04-(2.00+/-100.00)e-4-0.37 +/- 0.89DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off-2.5310.066-1.53 +/- 1.86-30.24 +/- 47.83No Violation Check
aoalpang -0.5110.292-13.79 +/- 25.32(1.63+/-27.20)e2DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 0.0230.0060.38 +/- 0.4942.42 +/- 22.99naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 -0.0030.006(9.01+/-4780.00)e-4-0.30 +/- 39.17naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 0.0010.0050.10 +/- 0.41-15.85 +/- 42.81naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 0.0140.0020.42 +/- 0.19-4.99 +/- 9.88naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang -0.4850.390-2.67 +/- 33.77-(1.62+/-3.56)e3DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 0.0230.0060.38 +/- 0.4945.56 +/- 22.94naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 -0.0030.006(8.19+/-4780.00)e-4-0.22 +/- 39.18naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 0.0010.0050.10 +/- 0.41-15.81 +/- 42.81naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 624.103266.627-(7.82+/-22.68)e3(1.88+/-2.92)e5KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 -353.961456.108-(7.90+/-3.88)e4-(2.60+/-65.20)e4KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 -636.972402.765(6.30+/-3.42)e4-(4.50+/-5.74)e5KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 0.0160.0090.12 +/- 0.7917.36 +/- 21.33KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 0.0070.0160.01 +/- 1.3914.59 +/- 23.78KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 -0.0290.014-0.15 +/- 1.22-13.77 +/- 21.91KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 -0.0153.344e-05-0.40 +/- 0.03-0.35 +/- 0.20naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 -0.0063.346e-050.84 +/- 0.01-0.03 +/- 0.06naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 -0.0023.015e-050.36 +/- 0.01-(1.53+/-0.19)e-9naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 9.496e-041.348e-04-0.01 +/- 0.010.56 +/- 0.96naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 -0.0024.269e-040.02 +/- 0.04-0.79 +/- 2.87naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 1.660e-043.260e-05-1.00 +/- 0.000.04 +/- 0.16naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 0.0240.0060.38 +/- 0.4933.45 +/- 22.72naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 -0.0050.006-0.02 +/- 0.487.67 +/- 39.18naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 0.0020.0050.11 +/- 0.41-2.63 +/- 43.14naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

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

Data Updated: Jul 21, 2026
Last Site Modification: Sep 30, 2021