In the SRGPS landing system, phase observables are uplinked to approaching aircraft where an integer ambiguity based double difference solution is computed. The probability of successful updates is sensitive to the number and quality of carrier phase observables. SRGPS must contend with rapidly changing multipath scatter and blockages from the ships structure. Antenna mounting limitations mandate multiple antenna diversity: System software must continuously select the best available signal path for each satellite. A post correlator diversity (PCD) approach has been developed for monitoring and weighting raw data prior to tracking loops by leveraging TISIs patented Integrated Demodulation/Navigation (IDN) processor. In contrast to conventional post loop diversity (PLD), this method responds before tracking loop damage can occur. PCD also offers J/S improvement. Phase biases induced by antenna lever errors are minimized by integrating ship flexure and IMU biases states. Beamformer diversity antenna elements are utilized for enhanced jamming margin and multipath rejection. Beamformer synthesis is based upon a proven military design. Integrity monitoring is provided over an independent ship-referenced path. In TISIs Phase I effort, both non-linear tracking simulations of the SRGPS shipside architecture and interfaces between TISIs PCD processor and Rockwell Collins beamformer are carried out.
Benefit: The post correlator diversity processor applies to all precise positioning and attitude determination applications subjected to blockage and multipath. Beyond aviation, construction vehicle guidance and control as well as marine docking guidance are important. Low earth orbit attitude determination and docking in space applications would benefit. PCD also applies to cellular communication station capacity improvement.
Keywords: Jamming, Jamming, tracking, beamforming, Multipath, aiding, SRGPS, phase, diversity