A detailed design of the receiver portion of a flight test model Interferometric Landmark Tracker (ILT) was completed. Prototype RF subassemblies and breadboard circuits were built and tested. Test results indicate the flight test model ILT receiver will provide an accuracy of 0.57 phase one sigma over the frequency range of 2.5 to 2.9 GHz, the specified temperature range of 30 F to +160 F and the received signal dynamic range of 50 dB. (Author)


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    Title :

    Autonomous Navigation Technology Phase 1B. ILT Flight Test Model Receiver Design


    Contributors:
    D. H. Aldrich (author) / L. O. Smith (author) / M. Rushanski (author)

    Publication date :

    1975


    Size :

    123 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English