Image dissector camera system study
Abstract
Various aspects of a rendezvous and docking system using an image dissector detector as compared to a GaAs detector were discussed. Investigation into a gimbled scanning system is also covered and the measured video response curves from the image dissector camera are presented. Rendezvous will occur at ranges greater than 100 meters. The maximum range considered was 1000 meters. During docking, the range, range-rate, angle, and angle-rate to each reflector on the satellite must be measured. Docking range will be from 3 to 100 meters. The system consists of a CW laser diode transmitter and an image dissector receiver. The transmitter beam is amplitude modulated with three sine wave tones for ranging. The beam is coaxially combined with the receiver beam. Mechanical deflection of the transmitter beam, + or - 10 degrees in both X and Y, can be accomplished before or after it is combined with the receiver beam. The receiver will have a field-of-view (FOV) of 20 degrees and an instantaneous field-of-view (IFOV) of two milliradians (mrad) and will be electronically scanned in the image dissector. The increase in performance obtained from the GaAs photocathode is not needed to meet the present performance requirements.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- March 1984
- Bibcode:
- 1984STIN...8420806H
- Keywords:
-
- Cameras;
- Comparison;
- Gallium Arsenides;
- Image Dissector Tubes;
- Infrared Imagery;
- Infrared Scanners;
- Orbital Rendezvous;
- Photocathodes;
- Spacecraft Docking;
- Spacecraft Tracking;
- Amplitude Modulation;
- Continuous Wave Lasers;
- Image Processing;
- Infrared Reflection;
- Mirrors;
- Range And Range Rate Tracking;
- Signal To Noise Ratios;
- Target Acquisition;
- Instrumentation and Photography