Back to Top

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
ai1ax1xon-0.0060.018-0.03 +/- 0.28-0.01 +/- 0.02DEG/SIRU-1 AXIS 1X ANALOG RATENo Violation Check
off0.0029.146e-04-3.96 +/- 0.09-0.02 +/- 0.02No Violation Check
ai1ax1yon-0.0050.018-0.03 +/- 0.28-0.02 +/- 0.02DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off0.0028.804e-04-3.98 +/- 0.09-0.01 +/- 0.01No Violation Check
ai1ax2xon0.0030.017-0.08 +/- 0.280.13 +/- 0.04DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off0.0029.193e-04-3.96 +/- 0.09-0.01 +/- 0.02No Violation Check
ai1ax2yon0.0030.017-0.05 +/- 0.280.08 +/- 0.04DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off0.0028.725e-04-3.98 +/- 0.09-0.01 +/- 0.01No Violation Check
ai2ax1xon0.0020.002-0.05 +/- 0.160.01 +/- 0.01DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off0.0140.027-3.88 +/- 0.05(0.00+/-0.00)e0No Violation Check
ai2ax1yon0.0030.002-0.04 +/- 0.160.01 +/- 0.01DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off-0.0030.013-3.92 +/- 0.02(0.00+/-0.00)e0No Violation Check
ai2ax2xon3.841e-040.002-0.05 +/- 0.160.01 +/- 0.01DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off1.606e-040.016-3.92 +/- 0.03(0.00+/-0.00)e0No Violation Check
ai2ax2yon8.887e-040.002-0.03 +/- 0.160.00 +/- 0.01DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off-0.0030.013-3.92 +/- 0.02(0.00+/-0.00)e0No Violation Check
aoalpang 1.1350.163-42.95 +/- 16.697.40 +/- 6.42DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 0.0400.004-0.39 +/- 0.430.17 +/- 0.18naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 0.0270.004-0.46 +/- 0.440.14 +/- 0.15naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 0.0250.004-0.50 +/- 0.410.15 +/- 0.18naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 0.0180.0020.15 +/- 0.210.10 +/- 0.09naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang 1.1960.148-46.00 +/- 15.294.64 +/- 5.60DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 0.0400.004-0.39 +/- 0.430.17 +/- 0.18naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 0.0270.004-0.46 +/- 0.440.16 +/- 0.15naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 0.0250.004-0.50 +/- 0.410.06 +/- 0.18naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 -1.754e+03217.569(7.42+/-22.40)e3(3.09+/-4.91)e3KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 -9.299e+03243.290-(8.82+/-3.02)e4(7.99+/-6.09)e3KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 4.698e+03406.103(3.16+/-4.23)e4(1.19+/-0.82)e4KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 -0.2720.021-1.14 +/- 2.210.65 +/- 0.52KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 0.1180.025-1.76 +/- 2.520.83 +/- 0.61KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 0.1340.020-1.61 +/- 2.020.81 +/- 0.44KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 -0.0080.0070.03 +/- 0.76-0.43 +/- 0.09naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 0.0170.0060.04 +/- 0.650.22 +/- 0.09naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 0.0070.0030.01 +/- 0.280.11 +/- 0.04naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 -0.0031.759e-04-0.03 +/- 0.020.01 +/- 0.01naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 -0.0035.803e-04-0.05 +/- 0.060.02 +/- 0.02naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 1.615e-051.268e-05-1.00 +/- 0.00-(1.10+/-2.34)e-4naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 0.0350.004-0.36 +/- 0.430.11 +/- 0.17naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 0.0250.004-0.43 +/- 0.430.17 +/- 0.15naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 0.0210.004-0.46 +/- 0.400.05 +/- 0.17naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

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

Data Updated: Aug 10, 2023
Last Site Modification: Sep 30, 2021