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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
off2.927e-042.122e-04-3.90 +/- 0.020.13 +/- 1.36No Violation Check
ai1ax1yon0.0150.106-0.96 +/- 1.62(2.04+/-1.97)e2DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off8.095e-051.187e-04-3.94 +/- 0.01-0.04 +/- 0.69No Violation Check
ai1ax2xon0.0010.106-0.94 +/- 1.62(1.93+/-1.97)e2DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off8.595e-051.510e-04-3.91 +/- 0.01-0.82 +/- 0.87No Violation Check
ai1ax2yon0.0150.106-0.96 +/- 1.62(2.00+/-1.97)e2DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off9.673e-051.115e-04-3.94 +/- 0.01-0.64 +/- 0.61No Violation Check
ai2ax1xon3.447e-051.669e-04-0.00 +/- 0.01-1.33 +/- 1.74DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off-2.4320.064-1.53 +/- 1.79-50.59 +/- 87.65No Violation Check
ai2ax1yon-3.036e-041.244e-04-(8.75+/-110.00)e-4-0.56 +/- 1.13DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off-2.5350.066-1.56 +/- 1.86-58.68 +/- 90.54No Violation Check
ai2ax2xon-1.175e-041.812e-04-0.01 +/- 0.021.07 +/- 1.85DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off-2.5160.066-1.55 +/- 1.85-55.90 +/- 89.76No Violation Check
ai2ax2yon-8.306e-051.036e-04-0.00 +/- 0.010.23 +/- 0.84DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off-2.5200.066-1.56 +/- 1.85-59.77 +/- 90.71No Violation Check
aoalpang 2.7020.267-16.79 +/- 24.97-(2.51+/-2.30)e3DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 -0.0060.004-0.02 +/- 0.3922.68 +/- 27.26naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 0.0130.0040.25 +/- 0.333.27 +/- 29.11naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 0.0300.0050.09 +/- 0.4813.82 +/- 30.73naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 -0.0020.0040.57 +/- 0.3228.18 +/- 22.64naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang -0.6240.407-11.84 +/- 37.10(2.35+/-3.72)e3DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 -0.0060.004-0.02 +/- 0.3922.69 +/- 27.26naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 0.0130.0040.25 +/- 0.333.25 +/- 29.13naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 0.0300.0050.09 +/- 0.4813.83 +/- 30.74naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 -445.267262.521-(9.78+/-23.41)e3-(1.50+/-0.41)e6KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 3.453e+03478.478-(6.80+/-4.32)e4(2.79+/-75.01)e4KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 -1.558e+03418.037(5.63+/-3.74)e4(2.17+/-0.68)e6KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 -0.0570.011-0.05 +/- 0.9525.73 +/- 31.56KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 8.272e-040.0180.13 +/- 1.57-46.16 +/- 36.25KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 0.0810.016-0.03 +/- 1.43-9.11 +/- 34.46KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 0.0093.175e-05-0.85 +/- 0.02-0.02 +/- 0.08naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 -0.0143.296e-05-0.48 +/- 0.030.03 +/- 0.18naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 -0.0063.205e-05-0.21 +/- 0.01-0.03 +/- 0.06naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 -0.0031.137e-04-0.01 +/- 0.01-0.56 +/- 0.80naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 0.0052.738e-040.01 +/- 0.031.56 +/- 1.53naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 5.581e-065.970e-06-1.00 +/- 0.00-(3.25+/-59.55)e-4naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 -0.0080.004-0.02 +/- 0.3923.55 +/- 27.53naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 0.0120.0040.25 +/- 0.3417.43 +/- 29.12naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 0.0290.0050.08 +/- 0.48-7.79 +/- 30.91naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

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

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