Michobo Twoja ignorancja jest już sławna na firstloox.org
raz
RNP 10 in oceanic and remote area:remote area:••With time limitation in IRS ONLY for With time limitation in IRS ONLY for aircraft without GPSaircraft without GPS••No time limitation with GPSNo time limitation with GPSRNP Enroute continental:RNP Enroute continental:••European BEuropean B--RNAV (5 NM accuracy)RNAV (5 NM accuracy)••US RNAV routes (QUS RNAV routes (Q--routes) 2 NM routes) 2 NM accuracyaccuracyQ-11Q-9Q-13Q-7Q-1Q-3Q-5Source FAASource FAARNP 4 (2) in oceanic and RNP 4 (2) in oceanic and remote area:remote area:••GPS requiredGPS requiredAll Airbus with an FMSAll Airbus with an FMScan fly these routescan fly these routes
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There are four Radio Altimeter antennae in aircraft
zone Z150 and two GPS antennae in Z233
Specified by Airbus specification ABS0912, two
variants are currently approved. ABS0912-01
is the Low range Radio Altimeter (LRRA)
antenna gasket and ABS0912-02, the GPS*
antenna gasket.
choć istotnie tu coś piszą, że do pasażerskich GPS nie bardzo aktualne no ale w takim razie ewidentnie w awionetkach mogą być
On Airbus aircraft, the HIL (Horizontal Integrity Limit) parameter is provided by the GPS (MMR – Multi Mode Receiver- or GPSSU –GPS on Airbus aircraft) through the IRS (Inertial Reference System) bus. Indeed, current transponders are not able to receive information directly from the GPS system, so the IRS is used as a “mail box” for GPS parameters (position, velocity, and HIL). The HIL parameter is transmitted on label 130 on this IRS bus (between IRS and transponder), and is used in the transponder to compute the value of NUCp (sent in BDS 0.5 and 0.6). All types of GPS installed on Airbus aircraft can transmit the HIL parameter on label 130. All Airbus EHS architectures provide HIL parameters to transponders.
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