Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 3483

x) 2t x e d f  S ³ Q( t Note The standard allowance for airb ay be used to bound the multipath errors ll be entical to the service provider ID in the FAS data block, except if ID equals 15 in the FAS data block. Note For S AS FAS data e data for validation of a cyclic redundancy chec is shown in At in that it contains the AS A and A for the p cted using S AS pseudo range be used If the service provider ID in the FAS data bloc e uals then S AS precise differential orrections cannot be used for the approach rrections, fast corrections and range rate corrections. c corrections. Note Two methods of computing ionospheric corrections are provided in and 3.5.8.4.3.3 The receiver shall apply a tropospheric model such that residual pseudo-range errors have a mean value ( ) less than 0.15 metres and a standard deviation less than 0.07 metres. Note A model was developed that meets this re uirement uidance is provided in Attachment D orne multipath defined in m 3.5.8.4.2.5 For precision approach and APV operations, the service provider ID broadcast Type 17 message sha id bloc s are stored in airborne databases The format of th t in achment D It differs from the AS FAS data bloc articular approach procedure For approaches condu S corrections the service provider ID in the FAS data bloc is the same as the service provider ID broadcast as part of the health and status information in Type message If the service provider ID in the FAS data bloc e uals then any service provider can c 3.5.8.4.3 Departure en route terminal and non precision approach operations 3.5.8.4.3.1 The receiver shall compute and apply long-term co 3.5.8.4.3.2 The receiver shall compute and apply ionospheri 23/11/06 A 2007/70/II. szám A endix Annex 10 — Aeronautical Communications 3.5.8.4.3.4 The receiver shall compute and apply horizontal and vertical protection levels as defined in 3.5.5.6. In this computation, stropo shall be: i 0.12 m 0.002 sin ( ) u  T here și is the elevation angle of the ith satellite. ition, ıair shall satisfy the condition that a normal distribution with zero mean and standard deviation equal to ıair the error distribution for residual aircraft pseudo-range errors as follows: w In add bounds n y y y f (x)dx Q for all 0 and f § · d t ¨ ¸ V V © ¹ ³ y nf (x)dx Q for all f y y  § · d t ¨ ¸ V V re fn(x) probability density function of the residual aircraft pseudo-range error and

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