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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 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
ai1ax1xon0.0050.105-0.96 +/- 1.60(1.86+/-1.94)e2DEG/SIRU-1 AXIS 1X ANALOG RATENo Violation Check
off7.796e-041.947e-04-3.90 +/- 0.020.50 +/- 1.03No Violation Check
ai1ax1yon0.0150.106-0.96 +/- 1.62(2.04+/-1.97)e2DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off9.523e-059.691e-05-3.94 +/- 0.010.45 +/- 0.44No Violation Check
ai1ax2xon0.0010.106-0.94 +/- 1.62(1.93+/-1.97)e2DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off7.908e-051.222e-04-3.91 +/- 0.010.46 +/- 0.54No Violation Check
ai1ax2yon0.0150.106-0.96 +/- 1.62(2.00+/-1.97)e2DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off2.941e-059.382e-05-3.94 +/- 0.010.19 +/- 0.42No Violation Check
ai2ax1xon1.283e-041.203e-04-0.00 +/- 0.010.16 +/- 1.08DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off-2.4320.064-1.53 +/- 1.79-50.59 +/- 87.65No Violation Check
ai2ax1yon-1.850e-041.006e-04-(6.53+/-90.00)e-40.12 +/- 0.79DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off-2.5350.066-1.56 +/- 1.86-58.68 +/- 90.54No Violation Check
ai2ax2xon-7.649e-051.281e-04-0.00 +/- 0.010.13 +/- 1.12DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off-2.5160.066-1.55 +/- 1.85-55.90 +/- 89.76No Violation Check
ai2ax2yon1.236e-055.580e-05-(7.03+/-50.00)e-40.05 +/- 0.42DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off-2.5200.066-1.56 +/- 1.85-59.77 +/- 90.71No Violation Check
aoalpang 1.7510.206-9.13 +/- 18.69-89.87 +/- 1716.58DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 -0.0860.0040.36 +/- 0.3831.33 +/- 15.59naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 0.0410.0040.35 +/- 0.3629.83 +/- 17.70naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 -0.0260.003-0.14 +/- 0.2633.50 +/- 12.02naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 0.0160.0020.58 +/- 0.19-14.64 +/- 11.12naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang -0.6990.275-23.24 +/- 24.50(1.70+/-1.88)e3DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 -0.0860.0040.36 +/- 0.3831.33 +/- 15.59naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 0.0410.0040.35 +/- 0.3629.83 +/- 17.69naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 -0.0260.003-0.14 +/- 0.2633.53 +/- 12.02naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 533.857267.911(1.51+/-2.35)e4-(1.05+/-0.36)e6KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 2.321e+03404.486-(8.64+/-3.57)e4(1.73+/-0.64)e6KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 -1.691e+03310.462(6.66+/-2.74)e4-(1.52+/-0.49)e6KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 -0.0710.016-0.07 +/- 1.36-(1.26+/-0.39)e2KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 0.0470.0170.16 +/- 1.50-4.64 +/- 32.92KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 -0.0460.013-0.14 +/- 1.14-4.07 +/- 25.71KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 -0.0123.402e-05-0.68 +/- 0.03-0.09 +/- 0.17naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 -0.0103.292e-050.68 +/- 0.02-0.07 +/- 0.11naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 -0.0043.284e-050.29 +/- 0.010.01 +/- 0.03naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 -1.337e-049.407e-05-0.00 +/- 0.01-0.03 +/- 0.60naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 -6.802e-042.587e-04-0.00 +/- 0.02-0.85 +/- 1.10naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 2.875e-051.720e-05-1.00 +/- 0.00(0.00+/-0.00)e0naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 -0.0850.0040.36 +/- 0.3825.84 +/- 15.89naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 0.0390.0040.35 +/- 0.3622.79 +/- 17.76naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 -0.0230.003-0.14 +/- 0.2730.90 +/- 12.21naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

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

Data Updated: Aug 10, 2023
Last Site Modification: Sep 30, 2021