Back to Top

PCADGRATE
Static Version: Max --- One Week

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

Delta/Yr below is a slope of the linear 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-0.0020.103-0.91 +/- 1.58(2.37+/-2.22)e2DEG/SIRU-1 AXIS 1X ANALOG RATENo Violation Check
off-0.0022.416e-04-3.86 +/- 0.02-1.23 +/- 1.41No Violation Check
ai1ax1yon-0.0010.104-0.92 +/- 1.60(2.31+/-2.24)e2DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off-0.0022.006e-04-3.89 +/- 0.020.84 +/- 1.17No Violation Check
ai1ax2xon-0.0040.104-0.92 +/- 1.60(2.35+/-2.24)e2DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off8.065e-061.422e-04-3.88 +/- 0.010.28 +/- 0.69No Violation Check
ai1ax2yon-0.0010.104-0.92 +/- 1.60(2.34+/-2.24)e2DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off-9.647e-051.524e-04-3.88 +/- 0.01-0.03 +/- 0.77No Violation Check
ai2ax1xon-3.836e-051.395e-04(8.35+/-130.00)e-4-1.48 +/- 1.41DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off-2.4240.063-1.49 +/- 1.78-17.74 +/- 46.48No Violation Check
ai2ax1yon1.275e-049.194e-05(6.84+/-900.00)e-50.86 +/- 0.80DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off-2.5140.066-1.54 +/- 1.85-26.72 +/- 47.61No Violation Check
ai2ax2xon1.035e-041.384e-04-(3.42+/-1300.00)e-5-0.67 +/- 1.30DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off-2.4870.065-1.53 +/- 1.83-26.77 +/- 47.14No Violation Check
ai2ax2yon4.119e-058.541e-05(6.93+/-80.00)e-40.11 +/- 0.55DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off-2.5310.066-1.53 +/- 1.86-30.24 +/- 47.83No Violation Check
aoalpang -0.1390.254-13.92 +/- 23.57-(2.46+/-20.55)e2DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 0.0610.0040.16 +/- 0.43-48.81 +/- 17.11naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 0.0340.0070.15 +/- 0.64-8.26 +/- 35.45naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 -0.0240.004-0.13 +/- 0.4139.64 +/- 26.38naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 0.0420.0020.33 +/- 0.23-18.32 +/- 16.52naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang 1.3730.351-9.65 +/- 32.69(1.21+/-2.55)e3DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 0.0610.0040.16 +/- 0.43-48.83 +/- 17.07naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 0.0340.0070.15 +/- 0.640.45 +/- 35.69naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 -0.0240.004-0.13 +/- 0.4139.65 +/- 26.38naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 -876.417260.796-(6.48+/-23.78)e3-(1.43+/-0.38)e6KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 3.618e+03462.217-(7.13+/-4.27)e4-(6.41+/-7.33)e5KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 -1.169e+03393.098(5.62+/-3.58)e4(2.64+/-0.64)e6KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 -0.0510.010-0.04 +/- 0.9516.55 +/- 32.28KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 -0.0190.0170.13 +/- 1.59-34.03 +/- 36.29KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 0.0840.015-0.01 +/- 1.41-20.21 +/- 33.39KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 -0.0163.159e-05-0.11 +/- 0.030.15 +/- 0.21naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 -0.0023.476e-050.91 +/- 0.01(5.41+/-0.52)e-9naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 -0.0022.891e-050.39 +/- 0.01(4.88+/-0.20)e-9naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 2.836e-071.054e-04-0.01 +/- 0.010.20 +/- 0.53naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 0.0023.333e-040.01 +/- 0.03-0.94 +/- 1.45naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 3.759e-052.170e-05-1.00 +/- 0.00-0.02 +/- 0.04naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 0.0620.0050.16 +/- 0.44-44.91 +/- 16.41naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 0.0310.0070.14 +/- 0.6411.09 +/- 35.85naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 -0.0230.004-0.12 +/- 0.4123.12 +/- 26.70naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

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

Data Updated: Jul 03, 2026
Last Site Modification: Sep 30, 2021