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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-4.063e-042.014e-04-3.90 +/- 0.02-1.41 +/- 1.23No Violation Check
ai1ax1yon0.0150.106-0.96 +/- 1.62(2.04+/-1.97)e2DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off-3.714e-051.169e-04-3.94 +/- 0.010.19 +/- 0.63No Violation Check
ai1ax2xon0.0010.106-0.94 +/- 1.62(1.93+/-1.97)e2DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off1.143e-051.429e-04-3.91 +/- 0.010.52 +/- 0.78No Violation Check
ai1ax2yon0.0150.106-0.96 +/- 1.62(2.00+/-1.97)e2DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off4.970e-051.085e-04-3.94 +/- 0.010.61 +/- 0.59No Violation Check
ai2ax1xon-1.361e-041.671e-04-0.00 +/- 0.02-0.35 +/- 1.79DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off-2.4320.064-1.53 +/- 1.79-50.59 +/- 87.65No Violation Check
ai2ax1yon-3.949e-041.225e-04-0.00 +/- 0.01-0.24 +/- 1.24DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off-2.5350.066-1.56 +/- 1.86-58.68 +/- 90.54No Violation Check
ai2ax2xon-2.688e-041.872e-04-0.01 +/- 0.02-1.43 +/- 1.98DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off-2.5160.066-1.55 +/- 1.85-55.90 +/- 89.76No Violation Check
ai2ax2yon-1.869e-048.785e-05-0.00 +/- 0.01-0.10 +/- 0.74DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off-2.5200.066-1.56 +/- 1.85-59.77 +/- 90.71No Violation Check
aoalpang 0.1750.280-15.50 +/- 26.11-(2.43+/-2.89)e3DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 0.0390.006-0.06 +/- 0.5391.02 +/- 26.89naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 0.0180.0030.38 +/- 0.29-21.59 +/- 30.02naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 0.0390.0040.00 +/- 0.397.22 +/- 19.64naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 0.0140.0020.53 +/- 0.20-20.79 +/- 14.60naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang 0.2760.362-11.89 +/- 33.81-(9.40+/-37.32)e2DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 0.0390.006-0.06 +/- 0.5391.10 +/- 26.89naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 0.0180.0030.38 +/- 0.29-21.56 +/- 30.02naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 0.0390.0040.00 +/- 0.397.18 +/- 19.64naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 -2.108e+03265.591-(1.14+/-2.47)e4-(2.49+/-3.79)e5KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 1.443e+03451.365-(6.55+/-4.15)e4-(2.92+/-0.73)e6KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 2.090e+03408.949(5.75+/-3.77)e4(2.32+/-0.65)e6KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 -0.0100.010-0.06 +/- 0.9440.29 +/- 30.37KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 -0.0910.0170.04 +/- 1.58-34.14 +/- 34.22KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 0.0720.0150.04 +/- 1.41-24.90 +/- 29.56KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 0.0022.742e-05-0.99 +/- 0.01-(6.72+/-0.36)e-9naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 -0.0163.147e-05-0.10 +/- 0.03-0.22 +/- 0.21naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 -0.0073.149e-05-0.04 +/- 0.01-0.01 +/- 0.07naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 -0.0021.454e-04-0.01 +/- 0.012.01 +/- 1.35naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 0.0054.143e-040.02 +/- 0.04-1.32 +/- 3.38naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 3.175e-042.509e-05-1.00 +/- 0.000.01 +/- 0.06naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 0.0400.006-0.06 +/- 0.5391.93 +/- 27.35naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 0.0160.0030.37 +/- 0.30-14.00 +/- 30.68naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 0.0390.0040.00 +/- 0.3923.30 +/- 20.00naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

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

Data Updated: Oct 04, 2026
Last Site Modification: Sep 30, 2021