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PCADGRATE
Static Version: Max --- Last Five years

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
ai1ax1xon0.0280.012-0.02 +/- 0.19-0.01 +/- 0.01DEG/SIRU-1 AXIS 1X ANALOG RATENo Violation Check
off1.128e-040.002-3.77 +/- 0.150.01 +/- 0.03No Violation Check
ai1ax1yon0.0290.012-0.02 +/- 0.19-0.01 +/- 0.01DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off8.281e-040.002-3.81 +/- 0.150.01 +/- 0.03No Violation Check
ai1ax2xon0.0170.0120.04 +/- 0.19-0.08 +/- 0.04DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off-3.368e-040.002-3.80 +/- 0.150.02 +/- 0.03No Violation Check
ai1ax2yon0.0210.0120.02 +/- 0.20-0.03 +/- 0.03DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off6.192e-040.002-3.81 +/- 0.150.01 +/- 0.03No Violation Check
ai2ax1xon-0.0017.521e-040.04 +/- 0.07-0.01 +/- 0.01DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off0.4070.762-2.94 +/- 1.47(0.00+/-0.00)e0No Violation Check
ai2ax1yon-0.0027.871e-040.03 +/- 0.08-0.01 +/- 0.01DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off0.4230.797-3.08 +/- 1.54(0.00+/-0.00)e0No Violation Check
ai2ax2xon0.0027.957e-040.03 +/- 0.08-0.01 +/- 0.01DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off0.4200.787-3.04 +/- 1.52(0.00+/-0.00)e0No Violation Check
ai2ax2yon0.0017.815e-040.02 +/- 0.08-0.00 +/- 0.01DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off0.4240.795-3.07 +/- 1.54(0.00+/-0.00)e0No Violation Check
aoalpang -3.6130.21028.32 +/- 21.48-8.14 +/- 7.45DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 -0.0240.0040.42 +/- 0.42-0.03 +/- 0.16naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 -0.0240.0050.40 +/- 0.45-0.00 +/- 0.16naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 -0.0340.0050.41 +/- 0.45-0.23 +/- 0.19naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 -0.0150.0020.65 +/- 0.22-0.12 +/- 0.09naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang -2.5850.25440.60 +/- 25.27-3.93 +/- 9.53DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 -1.652e+061.761e+06(3.20+/-171.80)e6-0.01 +/- 0.17naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 -0.0240.0050.40 +/- 0.450.04 +/- 0.16naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 -0.0350.0050.41 +/- 0.45-0.23 +/- 0.19naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 -4.007e+03135.726(3.85+/-1.51)e4-(4.60+/-3.41)e3KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 -1.556e+04444.970-(2.53+/-5.18)e4-(1.16+/-0.87)e4KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 -7.117e+03201.738(9.02+/-2.35)e4(1.63+/-4.48)e3KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 -0.1010.0050.50 +/- 0.520.02 +/- 0.09KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 0.0440.0090.98 +/- 0.88-0.25 +/- 0.23KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 -0.1570.0090.94 +/- 0.92-0.16 +/- 0.23KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 0.0020.0070.06 +/- 0.710.06 +/- 0.10naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 -0.0070.0070.02 +/- 0.650.34 +/- 0.09naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 -0.0030.0030.01 +/- 0.280.14 +/- 0.04naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 2.970e-049.701e-050.01 +/- 0.01-0.00 +/- 0.00naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 0.0045.758e-040.05 +/- 0.060.01 +/- 0.03naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 0.0025.416e-04-0.99 +/- 0.05(9.28+/-4099.00)e-6naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 -0.0170.0040.38 +/- 0.40-0.02 +/- 0.17naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 -0.0150.0040.37 +/- 0.43-0.06 +/- 0.15naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 -0.0310.0040.38 +/- 0.43-0.20 +/- 0.18naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

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

Data Updated: Jun 02, 2023
Last Site Modification: Sep 30, 2021