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PCADGRATE
Static Version: Min --- 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
ai1ax1xon0.0540.016-0.03 +/- 0.24-0.01 +/- 0.02DEG/SIRU-1 AXIS 1X ANALOG RATENo Violation Check
off0.0023.221e-04-3.96 +/- 0.04-0.00 +/- 0.01No Violation Check
ai1ax1yon0.0540.016-0.03 +/- 0.25-0.02 +/- 0.02DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off0.0022.053e-04-3.98 +/- 0.020.00 +/- 0.01No Violation Check
ai1ax2xon0.0610.016-0.07 +/- 0.240.13 +/- 0.04DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off0.0023.186e-04-3.97 +/- 0.030.00 +/- 0.01No Violation Check
ai1ax2yon0.0630.016-0.05 +/- 0.240.08 +/- 0.04DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off0.0011.991e-04-3.98 +/- 0.020.00 +/- 0.01No Violation Check
ai2ax1xon0.0030.002-0.06 +/- 0.190.01 +/- 0.01DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off999.0000.000e+00-3.91 +/- 0.00(0.00+/-0.00)e0No Violation Check
ai2ax1yon0.0050.002-0.05 +/- 0.190.01 +/- 0.01DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off999.0000.000e+00-3.94 +/- 0.03(0.00+/-0.00)e0No Violation Check
ai2ax2xon0.0030.002-0.05 +/- 0.190.02 +/- 0.01DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off999.0000.000e+00-3.94 +/- 0.03(0.00+/-0.00)e0No Violation Check
ai2ax2yon0.0030.002-0.03 +/- 0.190.01 +/- 0.01DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off999.0000.000e+00-3.94 +/- 0.03(0.00+/-0.00)e0No Violation Check
aoalpang 1.0530.149-43.31 +/- 16.173.39 +/- 6.20DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 0.0290.004-0.42 +/- 0.430.03 +/- 0.17naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 0.0460.004-0.46 +/- 0.440.12 +/- 0.14naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 0.0290.004-0.52 +/- 0.390.09 +/- 0.17naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 0.0220.0020.14 +/- 0.200.15 +/- 0.08naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang 1.2810.131-46.58 +/- 14.412.39 +/- 5.36DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 0.0290.004-0.42 +/- 0.430.04 +/- 0.17naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 0.0460.004-0.46 +/- 0.440.12 +/- 0.14naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 0.0290.004-0.52 +/- 0.390.08 +/- 0.17naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 587.714201.214(8.19+/-21.74)e3(3.53+/-4.60)e3KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 -1.128e+04231.032-(7.93+/-3.35)e4(7.16+/-5.85)e3KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 3.485e+03402.384(2.93+/-4.39)e4(1.34+/-0.77)e4KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 -0.1590.014-0.90 +/- 1.580.40 +/- 0.40KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 0.1360.023-1.81 +/- 2.520.83 +/- 0.58KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 0.1070.018-1.70 +/- 1.980.71 +/- 0.42KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 -0.0370.007-0.01 +/- 0.77-0.34 +/- 0.09naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 0.0120.0060.03 +/- 0.64-0.29 +/- 0.09naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 0.0050.0030.01 +/- 0.28-0.13 +/- 0.04naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 -0.0021.499e-04-0.03 +/- 0.020.00 +/- 0.01naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 -0.0025.344e-04-0.04 +/- 0.060.01 +/- 0.02naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 2.932e-051.213e-05-1.00 +/- 0.00-(1.44+/-2.50)e-4naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 0.0260.004-0.39 +/- 0.420.07 +/- 0.17naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 0.0450.004-0.42 +/- 0.430.12 +/- 0.14naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 0.0260.004-0.47 +/- 0.380.03 +/- 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