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PCADGRATE
Static Version: Mean --- Last Five years

One Week Three Month One Year Five Year Full Range Min Mean Max

Delta/Yr below is a slope of the liear 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
ai1ax1xon0.0450.014-0.02 +/- 0.210.01 +/- 0.01DEG/SIRU-1 AXIS 1X ANALOG RATENo Violation Check
off-0.0013.603e-04-3.90 +/- 0.040.00 +/- 0.01No Violation Check
ai1ax1yon0.0460.014-0.02 +/- 0.210.00 +/- 0.01DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off-5.474e-043.139e-04-3.93 +/- 0.030.00 +/- 0.01No Violation Check
ai1ax2xon0.0450.014-0.01 +/- 0.210.02 +/- 0.01DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off-7.587e-043.462e-04-3.91 +/- 0.040.00 +/- 0.01No Violation Check
ai1ax2yon0.0460.014-0.01 +/- 0.210.02 +/- 0.01DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off-6.696e-043.193e-04-3.93 +/- 0.03(7.52+/-95.65)e-4No Violation Check
ai2ax1xon4.023e-047.006e-04-0.00 +/- 0.080.00 +/- 0.00DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off999.0000.000e+00-3.77 +/- 0.01(0.00+/-0.00)e0No Violation Check
ai2ax1yon5.851e-047.220e-04-0.00 +/- 0.080.00 +/- 0.00DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off999.0000.000e+00-3.88 +/- 0.01(0.00+/-0.00)e0No Violation Check
ai2ax2xon4.721e-047.167e-04-0.01 +/- 0.080.00 +/- 0.00DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off999.0000.000e+00-3.85 +/- 0.01(0.00+/-0.00)e0No Violation Check
ai2ax2yon5.558e-047.212e-04-0.00 +/- 0.08(7.76+/-14.72)e-4DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off999.0000.000e+00-3.88 +/- 0.00(0.00+/-0.00)e0No Violation Check
aoalpang -0.1640.126-16.23 +/- 13.62-0.78 +/- 5.91DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 0.0030.0030.01 +/- 0.36-0.16 +/- 0.15naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 0.0280.004-0.04 +/- 0.400.03 +/- 0.13naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 -0.0020.003-0.06 +/- 0.350.04 +/- 0.16naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 0.0080.0020.42 +/- 0.180.11 +/- 0.07naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang 0.8260.172-17.71 +/- 18.67-8.95 +/- 6.85DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 -105.328219.250(4.35+/-236.50)e2-0.18 +/- 0.15naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 0.0280.004-0.04 +/- 0.400.03 +/- 0.13naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 -0.0030.003-0.06 +/- 0.35(4.69+/-1564.00)e-4naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 -1.557e+03158.216(2.62+/-1.73)e4-(2.80+/-3.02)e3KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 -1.431e+04302.803-(5.05+/-4.33)e4-(8.62+/-57.73)e2KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 -3.318e+03290.013(6.74+/-3.20)e4(3.15+/-4.96)e3KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 -3.489e-040.005-0.01 +/- 0.520.04 +/- 0.11KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 0.0190.0090.04 +/- 1.00-0.13 +/- 0.21KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 -0.0110.009-0.03 +/- 0.960.11 +/- 0.17KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 -0.0350.0070.00 +/- 0.71-0.32 +/- 0.09naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 0.0120.0060.04 +/- 0.64-0.32 +/- 0.09naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 0.0050.0030.02 +/- 0.28-0.14 +/- 0.04naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 -8.298e-045.552e-05-0.00 +/- 0.01(8.00+/-28.19)e-4naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 0.0012.320e-040.00 +/- 0.03-0.00 +/- 0.01naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 8.586e-052.204e-05-1.00 +/- 0.00-(3.34+/-8.52)e-4naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 0.0030.0030.01 +/- 0.36-0.17 +/- 0.15naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 0.0280.004-0.04 +/- 0.400.06 +/- 0.13naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 -0.0030.003-0.06 +/- 0.350.09 +/- 0.16naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

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

Data Updated: Nov 10, 2022
Last Site Modification: Sep 30, 2021