Table 4 Properties of the Swarm panel model used for aerodynamic and radiation pressure modeling
From: Swarm accelerometer data processing from raw accelerations to thermospheric neutral densities
Panel | Area | X | Y | Z |
|---|---|---|---|---|
Nadir 1 | 1.540 | 0.0 | 0.0 | 1.0 |
Nadir 2 | 1.400 | −0.19766 | 0.0 | 0.98027 |
Nadir 3 | 1.600 | −0.13808 | 0.0 | 0.99042 |
Solar array +Y | 3.450 | 0.0 | 0.58779 | −0.80902 |
Solar array −Y | 3.450 | 0.0 | −0.58779 | −0.80902 |
Zenith | 0.500 | 0.0 | 0.0 | −1.0 |
Front | 0.560 | 1.0 | 0.0 | 0.0 |
Side wall +Y | 0.753 | 0.0 | 1.0 | 0.0 |
Side wall −Y | 0.753 | 0.0 | −1.0 | 0.0 |
Shear panel nadir front | 0.800 | 1.0 | 0.0 | 0.0 |
Shear panel nadir back | 0.800 | −1.0 | 0.0 | 0.0 |
Boom +Y | 0.600 | 0.0 | 1.0 | 0.0 |
Boom −Y | 0.600 | 0.0 | −1.0 | 0.0 |
Boom zenith | 0.600 | −0.23924 | 0.0 | −0.97096 |
Boom nadir | 0.600 | 0.22765 | 0.0 | 0.97374 |