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![]() PPT33R wrote: I can't see that happening, especially when RNP is being deployed commercially. Boeing & Airbus are now certifying their newer airframes for RNP .1, which allegedly integrates GPS, INS, and DME into the FMS. The GPS portion requires RAIM and is much more reliable with WAAS. TIS, on the other hand, is a whole other issue... I am involved in the work being done with RNP. WAAS is not part of the calculus at all in the FMS sensor hierarcy for RNP_SAAAR instrument approach procedures. RNP 0.10 is acheived through complex interfaces of FMS software with GPS as the primary sensor. WAAS is not used. The most robust platforms (dual-thread aircraft, which will be a requirement where RNP is needed for the missed approach, use blended, updated IRU position along with GPS (or without GPS for a reasonable period of time in the event GPS suddently fails). WAAS's primary benefit is to provide the LPV glide-path for the LPV final approach segment. The RNP_SAAAR criteria's final approach segment glide-path is predicated on IFR-certified Baro VNAV. As an aside, when the FAA commissioned WAAS, they "dumbed down" the Baro VNAV criteria for public RNAV (GPS) IAPs, which increased existing VNAV minimums. This was a blatent political move to make LPV minimums look better. The assessment concets for the VNAV obstacle clearance surfaces in the RNP_SAAAR environment rightfully do an end-run around the dumbing down of public VNAV obstacle clearance criteria. |
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