Carrier phase differential GPS (DGPS) navigation architectures and algorithms for automatic shipboard landing of aircraft are described. Processing methodologies are defined to provide high integrity carrier phase cycle estimation and positioning by optimally exploiting the complementary benefits of measurement filtering and satellite geometric redundancy for the terminal navigation problem. Navigation performance sensitivity to the standard deviations of raw carrier and code phase measurement errors, measurement error correlation times, and the filtering duration is quantified. Necessary conditions to ensure acceptable terminal navigation availability are specifically defined.
Carrier phase navigation architecture for shipboard relative GPS
IEEE Transactions on Aerospace and Electronic Systems ; 42 , 2 ; 670-679
2006-04-01
2050255 byte
Article (Journal)
Electronic Resource
English
Carrier Phase Navigation Architecture for Shipboard Relative GPS
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