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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-1.718e-041.953e-04-3.90 +/- 0.020.85 +/- 1.22No Violation Check
ai1ax1yon0.0150.106-0.96 +/- 1.62(2.04+/-1.97)e2DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off-1.725e-049.966e-05-3.94 +/- 0.01-0.75 +/- 0.53No Violation Check
ai1ax2xon0.0010.106-0.94 +/- 1.62(1.93+/-1.97)e2DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off-3.067e-041.294e-04-3.91 +/- 0.01-0.39 +/- 0.68No Violation Check
ai1ax2yon0.0150.106-0.96 +/- 1.62(2.00+/-1.97)e2DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off-2.361e-041.007e-04-3.94 +/- 0.01-0.43 +/- 0.53No Violation Check
ai2ax1xon2.066e-041.465e-04-0.00 +/- 0.01-3.19 +/- 1.50DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off-2.4320.064-1.53 +/- 1.79-50.59 +/- 87.65No Violation Check
ai2ax1yon-3.804e-041.326e-04-0.00 +/- 0.010.58 +/- 1.28DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off-2.5350.066-1.56 +/- 1.86-58.68 +/- 90.54No Violation Check
ai2ax2xon-5.540e-041.432e-04-0.01 +/- 0.01-1.39 +/- 1.30DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off-2.5160.066-1.55 +/- 1.85-55.90 +/- 89.76No Violation Check
ai2ax2yon2.601e-041.216e-04-0.00 +/- 0.010.37 +/- 0.93DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off-2.5200.066-1.56 +/- 1.85-59.77 +/- 90.71No Violation Check
aoalpang 0.5700.279-12.52 +/- 26.04-(6.48+/-2.30)e3DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 0.0430.0050.47 +/- 0.43-17.24 +/- 23.20naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 -0.0320.0030.16 +/- 0.30-45.49 +/- 21.36naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 0.0340.0040.15 +/- 0.3844.99 +/- 31.18naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 -0.0190.0020.52 +/- 0.18-20.62 +/- 13.03naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang 0.3380.316-12.18 +/- 29.46(5.60+/-2.64)e3DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 0.0430.0050.47 +/- 0.43-17.28 +/- 23.20naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 -0.0320.0030.16 +/- 0.30-45.51 +/- 21.36naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 0.0340.0040.15 +/- 0.3844.92 +/- 31.17naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 1.564e+03248.584-(1.10+/-2.29)e4(6.11+/-28.33)e4KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 -1.517e+03424.725-(7.61+/-3.89)e4(1.42+/-0.61)e6KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 -1.216e+03377.840(6.46+/-3.46)e4-(1.19+/-0.54)e6KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 0.0080.0090.09 +/- 0.82-1.17 +/- 20.88KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 0.0510.015-0.09 +/- 1.38-6.34 +/- 23.92KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 -0.0440.013-0.08 +/- 1.222.77 +/- 21.86KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 -0.0113.199e-05-0.75 +/- 0.02-0.01 +/- 0.12naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 -0.0113.173e-050.61 +/- 0.02-0.03 +/- 0.11naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 -0.0053.080e-050.26 +/- 0.010.01 +/- 0.03naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 -1.948e-041.634e-04-0.01 +/- 0.011.65 +/- 1.15naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 0.0035.809e-040.03 +/- 0.05-3.92 +/- 3.49naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 -2.852e-044.398e-05-1.00 +/- 0.000.17 +/- 0.23naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 0.0410.0050.46 +/- 0.44-17.87 +/- 23.34naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 -0.0260.0030.15 +/- 0.30-45.78 +/- 20.75naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 0.0320.0040.15 +/- 0.3939.74 +/- 31.33naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

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

Data Updated: Aug 16, 2026
Last Site Modification: Sep 30, 2021