| 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 | Mean | RMS | Delta/Yr | Delta/Yr/Yr | Unit | Description | Limit Violation | |
|---|---|---|---|---|---|---|---|---|
| ai1ax1x | on | -9.936e-04 | 4.103e-04 | -0.01 +/- 0.17 | -(1.18+/-1.90)e-4 | DEG/S | IRU-1 AXIS 1X ANALOG RATE | No Violation | off | -0.004 | 4.789e-04 | -3.88 +/- 0.24 | (7.66+/-12.31)e-4 | No Violation |
| ai1ax1y | on | -0.001 | 4.121e-04 | -0.01 +/- 0.17 | -(1.30+/-15.97)e-5 | DEG/S | IRU-1 AXIS 1Y ANALOG RATE | No Violation | off | -0.005 | 4.817e-04 | -3.91 +/- 0.24 | (2.07+/-89.54)e-5 | No Violation |
| ai1ax2x | on | -5.230e-04 | 4.112e-04 | -0.01 +/- 0.17 | (8.69+/-28.06)e-5 | DEG/S | IRU-1 AXIS 2X ANALOG RATE | No Violation | off | -0.005 | 4.797e-04 | -3.88 +/- 0.24 | (6.80+/-11.73)e-4 | No Violation |
| ai1ax2y | on | -5.095e-04 | 4.131e-04 | -0.01 +/- 0.17 | (9.36+/-21.49)e-5 | DEG/S | IRU-1 AXIS 2Y ANALOG RATE | No Violation | off | -0.005 | 4.811e-04 | -3.90 +/- 0.24 | (4.21+/-9.30)e-4 | No Violation |
| ai2ax1x | on | 0.001 | 2.899e-04 | -0.01 +/- 0.15 | (4.50+/-18.08)e-5 | DEG/S | IRU-2 AXIS 1X ANALOG RATE | No Violation | off | 0.004 | 0.003 | -3.72 +/- 0.21 | -(5.27+/-160.20)e-4 | No Violation |
| ai2ax1y | on | 0.002 | 2.929e-04 | -0.01 +/- 0.16 | (6.20+/-18.02)e-5 | DEG/S | IRU-2 AXIS 1Y ANALOG RATE | No Violation | off | 6.649e-04 | 0.003 | -3.72 +/- 0.21 | -0.00 +/- 0.02 | No Violation |
| ai2ax2x | on | 0.001 | 2.919e-04 | -0.01 +/- 0.16 | -(1.51+/-na)e-6 | DEG/S | IRU-2 AXIS 2X ANALOG RATE | No Violation | off | 0.002 | 0.003 | -3.72 +/- 0.21 | -0.00 +/- 0.01 | No Violation |
| ai2ax2y | on | 0.002 | 2.927e-04 | -0.01 +/- 0.16 | -(4.40+/-14.06)e-5 | DEG/S | IRU-2 AXIS 2Y ANALOG RATE | No Violation | off | 9.068e-04 | 0.003 | -3.72 +/- 0.21 | -0.00 +/- 0.02 | No Violation |
| aoalpang | -0.501 | 0.020 | -12.80 +/- 14.00 | 0.28 +/- 0.46 | DEG | FSS ALPHA ANGLE MEAS | No Violation | |
| aoattqt1 | -0.001 | 5.334e-04 | 0.02 +/- 0.36 | -0.00 +/- 0.01 | na | ESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI) | No Violation | |
| aoattqt2 | -0.002 | 6.009e-04 | -0.03 +/- 0.41 | 0.01 +/- 0.01 | na | ESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI) | No Violation | |
| aoattqt3 | -0.001 | 5.383e-04 | -0.04 +/- 0.37 | 0.01 +/- 0.01 | na | ESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI) | No Violation | |
| aoattqt4 | -7.817e-04 | 2.728e-04 | 0.42 +/- 0.19 | 0.01 +/- 0.01 | na | ESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI) | No Violation | |
| aobetang | -0.176 | 0.031 | -16.88 +/- 21.50 | 0.27 +/- 0.69 | DEG | FSS BETA ANGLE MEAS | No Violation | |
| aocmdqt1 | -365.537 | 797.261 | (5.85+/-543.80)e3 | -0.01 +/- 0.01 | na | COMMANDED SPACECRAFT ATTITUDE QUATERNION 1 | No Violation | |
| aocmdqt2 | -0.002 | 6.004e-04 | -0.03 +/- 0.41 | 0.01 +/- 0.01 | na | COMMANDED SPACECRAFT ATTITUDE QUATERNION 2 | No Violation | |
| aocmdqt3 | -868.011 | 497.061 | (3.53+/-339.20)e3 | -(5.82+/-133.60)e-4 | na | COMMANDED SPACECRAFT ATTITUDE QUATERNION 3 | No Violation | |
| aoscpos1 | 1.791e+03 | 42.635 | (5.73+/-317.50)e2 | (6.02+/-1.71)e2 | KM | SPACECRAFT POSITION VECTOR X (ECI FRAME) | No Violation | |
| aoscpos2 | 27.669 | 72.939 | -(3.22+/-4.98)e4 | -(1.39+/-0.26)e3 | KM | SPACECRAFT POSITION VECTOR Y (ECI FRAME) | No Violation | |
| aoscpos3 | 1.095e+03 | 51.013 | (6.85+/-3.57)e4 | (2.46+/-2.23)e2 | KM | SPACECRAFT POSITION VECTOR Z (ECI FRAME) | No Violation | |
| aoscvel1 | -5.630e-04 | 8.591e-04 | -0.00 +/- 0.59 | 0.01 +/- 0.01 | KMPS | SPACECRAFT VELOCITY VECTOR X ECI FRAME) | No Violation | |
| aoscvel2 | 0.002 | 0.001 | 0.01 +/- 0.88 | -0.01 +/- 0.01 | KMPS | SPACECRAFT VELOCITY VECTOR Y (ECI FRAME) | No Violation | |
| aoscvel3 | -0.001 | 0.001 | -0.01 +/- 0.90 | 0.02 +/- 0.01 | KMPS | SPACECRAFT VELOCITY VECTOR Z (ECI FRAME) | No Violation | |
| aosunec1 | 0.004 | 0.001 | 0.00 +/- 0.71 | -0.00 +/- 0.01 | na | UNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME) | No Violation | |
| aosunec2 | 5.863e-04 | 9.474e-04 | 0.01 +/- 0.65 | 0.02 +/- 0.01 | na | UNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME) | No Violation | |
| aosunec3 | 2.522e-04 | 4.109e-04 | 0.00 +/- 0.28 | 0.01 +/- 0.00 | na | UNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME) | No Violation | |
| aosunsa1 | -2.355e-04 | 1.319e-05 | -0.00 +/- 0.01 | -(1.79+/-1.52)e-4 | na | CSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME X | No Violation | |
| aosunsa2 | 2.454e-04 | 2.385e-05 | 0.00 +/- 0.02 | -(1.88+/-4.83)e-4 | na | CSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME Y | No Violation | |
| aosunsa3 | 1.363e-06 | 8.089e-06 | -1.00 +/- 0.01 | (1.80+/-33.69)e-6 | na | CSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME Z | No Violation | |
| aotarqt1 | -0.001 | 5.324e-04 | 0.02 +/- 0.36 | -0.00 +/- 0.01 | na | TARGET ATTITUDE QUATERNION ELEMENT 1 | No Violation | |
| aotarqt2 | -0.002 | 5.993e-04 | -0.03 +/- 0.41 | 0.01 +/- 0.01 | na | TARGET ATTITUDE QUATERNION ELEMENT 2 | No Violation | |
| aotarqt3 | -0.001 | 5.372e-04 | -0.04 +/- 0.37 | 0.01 +/- 0.01 | na | TARGET ATTITUDE QUATERNION ELEMENT 3 | No Violation |
If you have any questions, please contact
swolk@cfa.harvard.edu.
Data Updated: Jun 02, 2023
Last Site Modification: Sep 30, 2021