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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
off8.106e-042.041e-04-3.90 +/- 0.02-0.20 +/- 1.26No Violation Check
ai1ax1yon0.0150.106-0.96 +/- 1.62(2.04+/-1.97)e2DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off1.210e-041.066e-04-3.94 +/- 0.01-0.92 +/- 0.49No Violation Check
ai1ax2xon0.0010.106-0.94 +/- 1.62(1.93+/-1.97)e2DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off2.017e-041.407e-04-3.91 +/- 0.01-0.57 +/- 0.68No Violation Check
ai1ax2yon0.0150.106-0.96 +/- 1.62(2.00+/-1.97)e2DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off1.239e-041.006e-04-3.94 +/- 0.01-0.04 +/- 0.49No Violation Check
ai2ax1xon1.585e-051.260e-04-0.00 +/- 0.01-1.69 +/- 1.18DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off-2.4320.064-1.53 +/- 1.79-50.59 +/- 87.65No Violation Check
ai2ax1yon2.807e-041.158e-04-0.00 +/- 0.010.30 +/- 1.00DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off-2.5350.066-1.56 +/- 1.86-58.68 +/- 90.54No Violation Check
ai2ax2xon3.132e-041.484e-04-0.01 +/- 0.01-1.17 +/- 1.40DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off-2.5160.066-1.55 +/- 1.85-55.90 +/- 89.76No Violation Check
ai2ax2yon-3.104e-057.617e-05-(9.23+/-70.00)e-40.47 +/- 0.55DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off-2.5200.066-1.56 +/- 1.85-59.77 +/- 90.71No Violation Check
aoalpang 0.0660.256-14.17 +/- 24.13(1.34+/-2.08)e3DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 -0.0030.0040.01 +/- 0.40-36.79 +/- 23.50naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 -6.523e-040.005-0.42 +/- 0.4839.04 +/- 33.17naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 0.0320.006-0.06 +/- 0.560.30 +/- 42.55naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 0.0010.0020.28 +/- 0.2114.64 +/- 11.92naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang 1.6590.310-22.37 +/- 29.43-(6.61+/-24.80)e2DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 -0.0030.0040.01 +/- 0.40-36.76 +/- 23.51naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 -6.401e-040.005-0.42 +/- 0.4839.01 +/- 33.18naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 0.0320.006-0.06 +/- 0.560.31 +/- 42.55naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 -2.312e+03266.893-(7.18+/-25.16)e3-(1.94+/-3.79)e5KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 1.299e+03438.909-(7.10+/-4.07)e4-(3.05+/-0.73)e6KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 2.007e+03382.821(5.68+/-3.57)e4(2.36+/-0.62)e6KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 -0.0040.011-0.07 +/- 1.0163.18 +/- 35.35KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 -0.0990.0170.04 +/- 1.60-34.60 +/- 34.73KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 0.0720.0150.04 +/- 1.37-32.16 +/- 31.51KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 -0.0083.209e-050.88 +/- 0.020.06 +/- 0.08naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 0.0143.125e-050.43 +/- 0.03-0.16 +/- 0.16naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 0.0063.110e-050.19 +/- 0.010.04 +/- 0.04naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 0.0011.180e-04-0.01 +/- 0.01-1.57 +/- 0.77naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 -0.0043.655e-040.01 +/- 0.042.64 +/- 1.51naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 -4.299e-042.941e-05-1.00 +/- 0.00-0.02 +/- 0.06naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 -0.0020.0040.00 +/- 0.40-47.68 +/- 23.58naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 0.0030.005-0.41 +/- 0.4843.99 +/- 33.87naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 0.0310.006-0.05 +/- 0.56-10.33 +/- 42.13naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

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

Data Updated: Apr 23, 2026
Last Site Modification: Sep 30, 2021