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PCADGRATE
Static Version: Max --- 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
ai1ax1xon0.0330.012-0.02 +/- 0.19-0.01 +/- 0.01DEG/SIRU-1 AXIS 1X ANALOG RATENo Violation Check
off-0.0040.001-3.77 +/- 0.14-0.02 +/- 0.02No Violation Check
ai1ax1yon0.0350.013-0.02 +/- 0.19-0.01 +/- 0.01DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off-0.0030.001-3.81 +/- 0.14-0.01 +/- 0.02No Violation Check
ai1ax2xon0.0240.0130.04 +/- 0.19-0.08 +/- 0.04DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off-0.0040.001-3.80 +/- 0.15-0.02 +/- 0.02No Violation Check
ai1ax2yon0.0260.0130.02 +/- 0.20-0.03 +/- 0.03DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off-0.0040.001-3.81 +/- 0.14-0.01 +/- 0.02No Violation Check
ai2ax1xon-0.0016.688e-040.04 +/- 0.07-0.02 +/- 0.01DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off999.0000.000e+00-3.64 +/- 0.08(0.00+/-0.00)e0No Violation Check
ai2ax1yon-0.0027.008e-040.03 +/- 0.08-0.01 +/- 0.01DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off999.0000.000e+00-3.81 +/- 0.07(0.00+/-0.00)e0No Violation Check
ai2ax2xon-5.615e-047.081e-040.03 +/- 0.08-0.01 +/- 0.01DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off999.0000.000e+00-3.77 +/- 0.07(0.00+/-0.00)e0No Violation Check
ai2ax2yon-1.204e-046.982e-040.02 +/- 0.07-0.00 +/- 0.01DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off999.0000.000e+00-3.80 +/- 0.08(0.00+/-0.00)e0No Violation Check
aoalpang -2.7300.18529.17 +/- 20.68-14.13 +/- 6.99DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 -0.0200.0040.44 +/- 0.41-0.33 +/- 0.15naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 -0.0030.0040.43 +/- 0.43-0.02 +/- 0.14naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 -0.0380.0040.42 +/- 0.43-0.17 +/- 0.18naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 -0.0070.0020.66 +/- 0.220.06 +/- 0.09naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang -2.4700.21841.70 +/- 24.06-15.53 +/- 8.71DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 -7.552e+051.572e+06(3.12+/-169.50)e6-0.34 +/- 0.16naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 -0.0030.0040.43 +/- 0.43-0.01 +/- 0.14naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 -5.2622.9106.19 +/- 313.98-0.24 +/- 0.18naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 -2.757e+03112.669(4.04+/-1.33)e4-(7.40+/-2.86)e3KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 -1.587e+04379.840-(1.52+/-5.17)e4-(1.04+/-0.86)e4KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 -8.122e+03178.739(9.51+/-2.51)e4-(5.24+/-44.94)e2KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 -0.1440.0060.59 +/- 0.700.01 +/- 0.09KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 0.0450.0070.93 +/- 0.75-0.28 +/- 0.20KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 -0.2000.0081.03 +/- 0.96-0.12 +/- 0.21KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 -0.0350.0070.01 +/- 0.71-0.39 +/- 0.09naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 0.0110.0060.04 +/- 0.64-0.27 +/- 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 2.550e-048.483e-050.01 +/- 0.01-0.00 +/- 0.00naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 0.0045.020e-040.05 +/- 0.06-(4.69+/-258.40)e-4naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 0.0014.967e-04-0.99 +/- 0.050.00 +/- 0.00naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 -0.0140.0040.40 +/- 0.40-0.30 +/- 0.16naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 0.0070.0040.39 +/- 0.420.02 +/- 0.14naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 -0.0320.0040.39 +/- 0.42-0.25 +/- 0.17naTARGET 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