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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-9.537e-042.167e-04-3.90 +/- 0.02-0.28 +/- 1.27No Violation Check
ai1ax1yon0.0150.106-0.96 +/- 1.62(2.04+/-1.97)e2DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off-2.769e-061.042e-04-3.94 +/- 0.01-0.31 +/- 0.55No Violation Check
ai1ax2xon0.0010.106-0.94 +/- 1.62(1.93+/-1.97)e2DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off4.223e-051.438e-04-3.91 +/- 0.01-0.69 +/- 0.79No Violation Check
ai1ax2yon0.0150.106-0.96 +/- 1.62(2.00+/-1.97)e2DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off-1.336e-051.001e-04-3.94 +/- 0.01-0.11 +/- 0.51No Violation Check
ai2ax1xon1.917e-051.104e-04-0.00 +/- 0.01-0.71 +/- 1.00DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off-2.4320.064-1.53 +/- 1.79-50.59 +/- 87.65No Violation Check
ai2ax1yon-1.796e-041.197e-04-(8.18+/-110.00)e-40.38 +/- 0.95DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off-2.5350.066-1.56 +/- 1.86-58.68 +/- 90.54No Violation Check
ai2ax2xon-2.981e-041.425e-04-0.01 +/- 0.01-0.18 +/- 1.25DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off-2.5160.066-1.55 +/- 1.85-55.90 +/- 89.76No Violation Check
ai2ax2yon-1.202e-048.553e-05-(7.43+/-80.00)e-40.03 +/- 0.53DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off-2.5200.066-1.56 +/- 1.85-59.77 +/- 90.71No Violation Check
aoalpang 0.5130.257-11.04 +/- 23.39(2.21+/-1.62)e3DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 -0.0740.0030.32 +/- 0.34-18.97 +/- 12.51naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 0.1100.006-0.13 +/- 0.603.50 +/- 27.41naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 -0.0390.005-0.18 +/- 0.4642.02 +/- 22.98naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 -0.0250.0010.36 +/- 0.14-13.25 +/- 9.28naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang -0.7340.291-17.38 +/- 26.49(1.58+/-1.90)e3DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 -0.0740.0030.32 +/- 0.34-15.08 +/- 12.52naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 0.1100.006-0.13 +/- 0.603.53 +/- 27.41naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 -0.0390.005-0.18 +/- 0.4641.99 +/- 22.98naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 -1.896e+03274.999-(7.81+/-24.80)e3-(3.63+/-3.92)e5KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 1.635e+03460.704-(6.96+/-4.12)e4-(2.76+/-0.76)e6KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 1.446e+03403.972(5.62+/-3.61)e4(2.15+/-0.65)e6KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 -0.0120.011-0.07 +/- 0.9941.76 +/- 35.36KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 -0.0860.0180.06 +/- 1.61-35.43 +/- 36.95KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 0.0730.0160.04 +/- 1.39-38.44 +/- 33.61KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 -0.0163.228e-050.32 +/- 0.030.00 +/- 0.20naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 0.0053.483e-050.87 +/- 0.010.03 +/- 0.04naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 0.0022.952e-050.38 +/- 0.01(3.36+/-0.13)e-9naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 -0.0011.316e-04-0.01 +/- 0.01-1.79 +/- 0.79naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 0.0044.778e-040.02 +/- 0.043.71 +/- 1.97naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 -8.682e-053.395e-05-1.00 +/- 0.00-0.03 +/- 0.05naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 -0.0720.0030.32 +/- 0.34-8.56 +/- 12.86naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 0.1100.006-0.13 +/- 0.608.97 +/- 28.04naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 -0.0380.005-0.18 +/- 0.4642.84 +/- 23.61naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

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

Data Updated: Jun 07, 2026
Last Site Modification: Sep 30, 2021