Back to Top

PCADGRATE
Static Version: Min --- 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
ai1ax1xon0.0050.105-0.96 +/- 1.60(1.86+/-1.94)e2DEG/SIRU-1 AXIS 1X ANALOG RATENo Violation Check
off3.284e-042.070e-04-3.90 +/- 0.020.58 +/- 1.35No Violation Check
ai1ax1yon0.0150.106-0.96 +/- 1.62(2.04+/-1.97)e2DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off-4.938e-051.124e-04-3.94 +/- 0.010.07 +/- 0.59No Violation Check
ai1ax2xon0.0010.106-0.94 +/- 1.62(1.93+/-1.97)e2DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off-1.690e-041.363e-04-3.91 +/- 0.010.33 +/- 0.73No Violation Check
ai1ax2yon0.0150.106-0.96 +/- 1.62(2.00+/-1.97)e2DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off-5.196e-051.039e-04-3.94 +/- 0.010.50 +/- 0.57No Violation Check
ai2ax1xon2.183e-041.712e-04-0.00 +/- 0.020.15 +/- 1.80DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off-2.4320.064-1.53 +/- 1.79-50.59 +/- 87.65No Violation Check
ai2ax1yon2.272e-041.034e-04(1.63+/-90.00)e-4-0.71 +/- 0.90DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off-2.5350.066-1.56 +/- 1.86-58.68 +/- 90.54No Violation Check
ai2ax2xon3.141e-041.742e-04-0.01 +/- 0.02-1.25 +/- 1.79DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off-2.5160.066-1.55 +/- 1.85-55.90 +/- 89.76No Violation Check
ai2ax2yon2.693e-049.101e-05-(2.96+/-80.00)e-4-0.50 +/- 0.72DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off-2.5200.066-1.56 +/- 1.85-59.77 +/- 90.71No Violation Check
aoalpang -0.0940.268-17.55 +/- 24.55-(1.29+/-2.56)e3DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 0.0130.0060.28 +/- 0.5618.31 +/- 35.05naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 8.208e-040.0030.27 +/- 0.28-0.43 +/- 19.58naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 8.623e-040.0050.09 +/- 0.47-46.38 +/- 32.83naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 0.0250.0030.38 +/- 0.27-18.84 +/- 14.83naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang -2.6640.396-11.37 +/- 36.67-76.69 +/- 3694.03DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 0.0130.0060.28 +/- 0.5618.27 +/- 35.05naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 8.264e-040.0030.27 +/- 0.28-0.43 +/- 19.57naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 8.733e-040.0050.09 +/- 0.47-46.37 +/- 32.83naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 -742.388264.081-(9.04+/-23.71)e3-(1.56+/-0.41)e6KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 3.693e+03475.894-(6.85+/-4.33)e4-(5.54+/-7.36)e5KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 -1.324e+03410.455(5.62+/-3.69)e4(2.79+/-0.67)e6KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 -0.0580.011-0.05 +/- 0.9641.22 +/- 31.74KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 -0.0160.0170.10 +/- 1.56-35.89 +/- 36.93KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 0.0910.016-0.01 +/- 1.42-17.83 +/- 33.03KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 -0.0022.972e-05-1.00 +/- 0.01(6.35+/-0.30)e-9naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 -0.0163.241e-050.08 +/- 0.030.10 +/- 0.21naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 -0.0073.231e-050.03 +/- 0.010.03 +/- 0.07naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 2.581e-041.290e-04-0.01 +/- 0.011.52 +/- 1.00naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 4.944e-042.372e-040.01 +/- 0.020.14 +/- 1.53naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 1.618e-051.080e-05-1.00 +/- 0.00-0.01 +/- 0.04naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 0.0140.0060.28 +/- 0.562.09 +/- 34.63naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 0.0020.0030.27 +/- 0.284.75 +/- 19.82naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 0.0020.0050.09 +/- 0.48-30.03 +/- 33.22naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

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

Data Updated: Sep 23, 2026
Last Site Modification: Sep 30, 2021