Function of Component
Sun sensors detect the position of the sun and are used for attitude control. They are considered one of the “sensors & inputs” in the ADCS architecture. For more information, refer to Sun Sensors
Key Parameters
- Field of View (FOV)
- Accuracy
- Accuracy in this context refers to how correct the sun sensor’s measurement of the sun’s angle to the sensor’s normal is.
- For the 2023 competition cycle, the primary payload required a pointing accuracy of 1-1.5 degrees while the secondary payload required a pointing accuracy of 0.1-0.2 degrees.
- Sampling Rate
- Sampling rate in this context refers to the frequency at which the sensor makes readings.
- For ADCS applications, the more information available, the more accurate a picture can be made regarding the satellite’s orientation. So, a higher frequency is generally more desirable.
- Size
- Size in this context refers to the overall volume of the device as well as each individual major axis dimension.
- Ideally, the device should be as compact as possible, on the order of 20-40 mm for its length and width and <10 mm for its height.
- Weight
- Weight in this context refers to the overall weight of the device.
- Since the entire spacecraft for the 2023 cycle needs to be within 4kg, the device should not take up a significant portion of that weight.
- Input Voltage
- Input voltage in this context refers to the amount of supplied voltage that the device requires.
- For the 2023 cycle spacecraft, the input voltage should be between 1 and 5 V, depending on its current draw.
- Input Power
- Input power in this context refers to the amount of supplied power that the device requires.
- For the 2023 cycle spacecraft, the input power must be less than 5W.
Selection Criteria
- Field of View (FOV)
- Accuracy
- Between 0.1 and 1.5 degrees
- Sampling Rate
- Size
- Length less than 90 mm
- Width less than 90 mm
- Diameter (if applicable) less than 90 mm
- Height less than 10 mm
- Weight
- Input Voltage
- Input Power
Final Selection
The following part was selected: SS200 from AAC Clyde Space (see sources for datasheet).