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

Abstract

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)

Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1975
Accession Number
ADA019414

Entities

People

  • Douglas H. Aldrich
  • Lynn O. Smith
  • Michael Rushanski

Organizations

  • International Business Machines Corporation (Armonk, NY)

Tags

DTIC Thesaurus Topics

  • Accuracy
  • Autonomous Navigation
  • Dynamic Range
  • Frequency
  • Models
  • Navigation

Fields of Study

  • Engineering

Readers

  • Aerospace Test and Evaluation
  • Radio communications and signal processing.