Star and sun sensor for attitude and position control

Optics: measuring and testing – Angle measuring or angular axial alignment – With photodetection remote from measured angle

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Details

33249, G01B 1126, G01C 100, F41G 138

Patent

active

046182594

ABSTRACT:
A combined sun and star sensing system for attitude and position control of a space vehicle, includes a star image sensor having a first objective and a first detector array arranged in the focal plane, the objective being constructed for a well defined aberration so as to convert a point like object into a defined spot or area having a diameter larger than the diameter of an element of the detector array; the sun sensor has a regular objective and a second detector array is arranged in the image plane of that objective sun sensor; the two detector arrays have similar and a similar number of detector elements, and are alternately connected to a single evaluating electronic.

REFERENCES:
patent: 3744913 (1973-07-01), Farthing et al.
patent: 3931515 (1976-01-01), Parkin
patent: 4225781 (1980-09-01), Hammons
patent: 4367403 (1983-01-01), Miller

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