Attitude Determination and Control System - CalgaryToSpace/CTS-SAT-1-Wiki GitHub Wiki
Attitude Determination & Control System
The Attitude Determination & Control System is used to determine and control the attitude of the satellite via a negative feedback loop.
Model: CubeSpace Gen 1 ADCS
The ADCS selected is able to complete the 90-degree rotation maneuver required by the CTS-SAT-1 mission.
Subteams That Affect It
These are the subsystems & their relevant subteams that affect the performance of the Attitude Determination & Control System:
Subteams That Are Affected By It
These are the subsystems & their relevant subteams that are affected by the performance of the Attitude Determination & Control System:
Sun Pointing Faces
| -Z | +Y |
|---|---|
| Sun/Zenith | Opposite Pin Header |
Coarse Sun Sensor Mappings
| CSS # | CubeSpace Coordinate | CTS Coordinate |
|---|---|---|
| 1 | +X (MPI); toward Nadir side | +Z |
| 2 | +X (MPI); toward Zenith side | +Z |
| 3 | -Y (Pin Header) | +X |
| 4 | +Y (Not Pin Header) | -X |
| 5 | -Z (Sun/Zenith); toward Antenna | +Y |
| 6 | -X (Antenna); inner | -Z |
| 7 | +Z (Boom/Nadir) | -Y |
| 8 | -Z (Sun/Zenith) | +Y |
| 9 | -X (Antenna/Inner) | -Z |