A kind of sun sensor is designed based on the optical fiber. This project consists of three parts: optical head, photoelectric
sensor and signal processing unit. The innovation of this design lies in the improvement of traditional sun sensor, where
multi-fibers, used as a leader, are symmetrically distributed on the surface of a spacecraft. To determine the attitude of a
spacecraft, the sun sensor should measure the direction of the sun. Because the fiber length can be adjusted according to
the fact, photoelectric sensor can be placed deeply inside a spacecraft to protect the photoelectric sensor against the
damage by the high-energy particles from outer space. The processing unit calculates the difference value of sun energy
imported by each pair of opposite optical fiber so as to obtain the angle and the orientation between the spacecraft and
the sun. This sun sensor can suit multi-field of view, both small and large. It improves the accuracy of small field of view
and increases the precision of locating a spacecraft. This paper briefly introduces the design of processing unit. This sun
sensor is applicable to detect the attitude of a spacecraft. In addition, it can also be used in solar tracking system of PV
technology.
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