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Abstract:
This report describes a systems-level design of a data link that enables a high velocity missile to receive guidance commands from a 35 GHzRadar. The objectives for this design include a Bit Error Rate (BER) of 10-6 at 1 km downrange, low power consumption, and miniaturized components so that the data link can fit on the back of a missile. No custom designed electronic chips are necessary. The design assumes the implementation of Boolean equations for Cyclic Redundance checking (CRC) on a programmable logic device. The report concludes that based on a simple rainfall attenuation model, the system can meet the BER performance objective in moderate rain.
| Limitations: |
 APPROVED FOR PUBLIC RELEASE |
| Description: |
Final rept. Dec 1999-June 2000 |
| Pages: |
53 |
| Report Date: |
SEP 2001 |
| Report Number: |
A663793 |
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Keywords relating to this report:
