Star detection and tracking using CCDs
Abstract
The design and operation of a star sensor using a CCD imaging array and microprocessor-based data acquisition and processing are briefly discussed. The estimated absolute accuracy of the instrument is 0.1 of the pixel size, corresponding to about 4 arcsec for the present 4 x 3-deg field of view. The use of a light intensifier stage will increase the sensor instrument sensitivity by about a factor of 100. A similar increase in sensitivity can be achieved through a more intense cooling of the detector to allow for larger integration times. The use of a microprocessor for data acquisition, management, and processing makes it possible to adapt the sensor to various mission requirements by simply modifying the software.
- Publication:
-
Automatic Control in Space 1982
- Pub Date:
- 1983
- Bibcode:
- 1983aucs.proc..289B
- Keywords:
-
- Attitude Control;
- Charge Coupled Devices;
- Spacecraft Control;
- Star Trackers;
- Algorithms;
- Computer Programs;
- Microprocessors;
- Onboard Data Processing;
- Spacecraft Electronic Equipment;
- Spacecraft Instrumentation