Back to Top

PCADGRATE
Static Version: Min --- Full Range

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
ai1ax1xon0.0016.737e-04-0.05 +/- 0.28(2.12+/-15.16)e-4DEG/SIRU-1 AXIS 1X ANALOG RATENo Violation Check
off-0.0054.718e-04-3.94 +/- 0.230.00 +/- 0.00No Violation Check
ai1ax1yon0.0026.549e-04-0.05 +/- 0.270.00 +/- 0.00DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off-0.0064.703e-04-3.96 +/- 0.230.00 +/- 0.00No Violation Check
ai1ax2xon-2.160e-046.962e-04-0.07 +/- 0.29(1.11+/-18.26)e-4DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off-0.0054.693e-04-3.94 +/- 0.230.00 +/- 0.00No Violation Check
ai1ax2yon7.895e-046.708e-04-0.06 +/- 0.280.00 +/- 0.00DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off-0.0064.725e-04-3.96 +/- 0.230.00 +/- 0.00No Violation Check
ai2ax1xon0.0014.105e-04-0.06 +/- 0.220.00 +/- 0.00DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off-0.0110.002-3.75 +/- 0.15-0.01 +/- 0.04No Violation Check
ai2ax1yon0.0024.189e-04-0.05 +/- 0.220.00 +/- 0.00DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off-0.0130.002-3.76 +/- 0.150.01 +/- 0.03No Violation Check
ai2ax2xon0.0024.163e-04-0.06 +/- 0.220.00 +/- 0.00DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off-0.0110.002-3.74 +/- 0.15-(1.10+/-289.70)e-4No Violation Check
ai2ax2yon0.0024.173e-04-0.04 +/- 0.220.00 +/- 0.00DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off-0.0130.003-3.75 +/- 0.16-0.01 +/- 0.04No Violation Check
aoalpang -1.0950.028-35.96 +/- 20.360.15 +/- 0.55DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 -0.0046.243e-04-0.40 +/- 0.420.01 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 -0.0046.477e-04-0.43 +/- 0.440.01 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 -0.0045.941e-04-0.49 +/- 0.400.03 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 0.0730.058-0.24 +/- 38.790.01 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang -0.4310.025-43.95 +/- 17.270.12 +/- 0.47DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 -0.0046.246e-04-0.40 +/- 0.420.01 +/- 0.01naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 -0.0046.477e-04-0.43 +/- 0.440.01 +/- 0.01naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 -0.0045.938e-04-0.49 +/- 0.400.01 +/- 0.01naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 2.551e+0338.843-(2.26+/-3.17)e4(9.44+/-2.43)e2KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 -2.804e+045.423e+04-(4.44+/-365.20)e576.72 +/- 291.60KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 1.318e+0366.221(2.55+/-4.55)e4(1.65+/-0.39)e3KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 0.0360.002-1.06 +/- 1.640.02 +/- 0.02KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 -0.0250.003-1.39 +/- 1.780.07 +/- 0.02KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 -0.0370.002-1.50 +/- 1.490.10 +/- 0.02KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 0.0020.001-0.01 +/- 0.730.01 +/- 0.01naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 -5.110e-049.614e-04-0.00 +/- 0.650.01 +/- 0.01naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 4.830e-044.139e-04-0.01 +/- 0.280.01 +/- 0.00naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 -8.351e-042.112e-05-0.02 +/- 0.01(7.30+/-4.04)e-4naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 -0.0026.992e-05-0.03 +/- 0.05(6.02+/-13.50)e-4naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 5.028e-061.107e-06-1.00 +/- 0.00(0.00+/-0.00)e0naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 -0.0046.134e-04-0.36 +/- 0.410.01 +/- 0.01naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 -0.0036.438e-04-0.40 +/- 0.430.01 +/- 0.01naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 -0.0035.798e-04-0.45 +/- 0.390.02 +/- 0.01naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

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

Data Updated: Mar 31, 2023
Last Site Modification: Sep 30, 2021