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CubeSat Sun Sensor
 
 

 

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  • Overview
  • Technical Details
  • Photo's
  • Datasheet

The cubesat sun sensor determines the spacecraft body angles with respect to the sun. The sensor is extremely small and light to minimise the demands on nano-spacecraft. The sensor achieves much higher measurement accuracy than traditional photodiode cosine sensors.

The sensor consists of a CMOS PSD detector sitting behind a small pin-hole with a field of view of +/- 60 degrees. The device produces four analogue voltages that are dependant on the incident angle of sunlight in the horizontal and vertical directions. Each sensor is supplied with a calibration algorithm that calculates the sun vector from these four voltages to an accuracy of +/-0.2 degrees.

FUNCTIONAL CHARACTERISTICS

  • Field of view: 120°
  • Update Rate: > 10 Hz (limited by ADC)
  • Accuracy: < 0.5°

PHYSICAL CHARACTERISTICS

  • Mass: < 5 g
  • Power: < 5 mA
  • Size: 33mm x 11mm x 6mm

ENVIRONMENTAL SPECIFICATIONS

  • Operating temperature: -25°C to +50°C
  • 25g rms random, 5000g shock
  • 10krad total dose (component level)

INTERFACES

  • Power Supply: 3.3 or 5 V
  • I/F: 4 analogue channels, 9-way Nano-D connector

FEATURES

  • PSD architecture
  • Good accuracy
  • Wide field of view
  • Ultra Small size and low mass
  • Low power
  • Simple analogue interface

APPLICATIONS

  • Accurate determination of sun-angle
  • Four to six sensors can achieve full sky coverage
  • Used in conjunction with a magnetometer for simple attitude control
  • Can be used as safe-mode sensors on gyro or star-mapper controlled systems

 

 

Click on the image to download the datasheet.