Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 3492

i); ı_H12 i v (LP ssu ing that a latent fault exists in one, and only one reference re VPLH1 max VPLj N i 1 ¦ N i 1 ¦  B_ N i 1 ¦ N i 1 ¦ i i M U § · ¨ ¸ © ¹ ı2 pr_gnd,i ı2 pr_air,i ı2 tropo,i ı2 iono,i; Mi the number of reference receivers used to compute the pseudo-range corrections for the ith ranging source (indicated by the B values); and Ui the number of reference receivers used to compute the pseudo-range corrections for the ranging source, excluding the jth reference receiver. Note A latent fault includes any erroneous measurement(s) that is not immediately detected by the ground subsystem such that the broadcast data are affected and there is an induced position error in the aircraft subsystem 3.6.5.5.1.3 Definition of multipliers for Category I precision approach and AP The multipliers are given in Table B-67. 3.6.5.5.2 AS positioning service The signal-in-space horizontal protection level is an upper confidence bound on e horizontal error in the position relative to the GBAS reference point defined as: ith th HPL MAX HPLH0,HPLH1 23/11/06 A 2007/70/II. szám A endix Annex 10 — Aeronautical Communications able multipliers for Category precision approac and A Mi Multiplier 1(Note) Kffmd 6.86 5.762 5.81 5.847 Kmd Not used 2.935 2.898 2.878 Note For AP I approaches supported by Type messages broadcast without the parameter bloc 3.6.5.5.2.1 Normal measurements conditions. The horizontal protection level (HPLH0), assuming that normal measurement conditions (i.e. no faults) exist in all reference receivers and on all ranging sources, is calculated as: HPLH0 Kffmd, POS d major where: x y x y major xy d d d d d d § ·    © ¹ i i sy,i the partial derivative of position error in the y-direction with respect to pseudo-range error on the ith satellite Kffmd,POS the multiplier derived from the probability of fault-free missed detection N the number of ranging so i the ranging s used in the position solution ıi the pseudo-ran n 3.6.5.5.1.1 Note For the AS positio x and y axes define an arbit onal basis in the hori ontal plane 3.6.5.5.2.2 Faulted measur When the Type B parameter blocks, the alue for HPLH1 is defined as zero. Otherwise, the horizontal protection le ing that a latent fault exists in and only one reference receiver, is: HPLH1 max HPLj  ¨ ¸ ¨ ¸ N x x,i i 1 d s V ¦ N d s V ¦ y y,i i 1 N x,i y,i i d s s V ¦ xy i 1 sx,i the partial derivative of position error in the x-direction with respect to pseudo-range error on the ith satellite urces used in the position solution source index for ranging source ge error term as defined i ning service the rary orthog ement conditions 101 me without ssage is broadcast vel (HPLH1), assum v one A 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I where HPLj for j 1 to 4 is: zj Kmd_POS d major,H1 and HPLj B_hor N N j x,i i,j i 1 S B § · § · ¨ ¸ © ¹ ¦ the jth reference receiver measurement for the ith ranging source. md tem is faulted. y,i i,j i 1 S B ¨ ¸ © ¹ ¦ B_horz Bi,j the broadcast differences between the broadcast pseudo-range corrections and the corrections obtained excluding K _POS the multiplier derived from the probability of missed detection given that the ground subsys x y x y major,H1 xy d_H1 d_H1 d_H1 d_H1 d d_H1 § ·     ¨ ¸ ¨ ¸ i i Note For the AS positioning service the x and y axes define an arbitrary orthogonal basis in the hori ontal plane © ¹ N x x,i i 1 d_H1 s _H1 V ¦ N y y,i i 1 d_H1 s _H1 V ¦ N xy x,i y,i i i 1 d_H1 s s _H1 V ¦ i i pr_gnd,i pr_air,i tropo,i iono,i i M _H1 U § · V V  V  V  V ¨ ¸ © ¹ Mi the number of reference receivers used to compute the pseudo-range corrections for the ith ranging source (indicated by the B values). the number of reference receivers used to compute the pseudo-range corrections for the ith ranging source, excluding the jth reference receiver. Note A latent fault includes any erroneous measurement(s) that is not immediately detected by the ground subsystem such that the broadcast data are affected and there is an induced position error in the aircraft subsystem 3.6.5.5.2.3 Definition of multipliers for AS positioning service The multiplier Kffmd_POS is equal to 10.0 and the multiplier Kmd_POS, is equal to 5.3. .6.5.6 A ERT IMITS Note uidance concerning the calculation of alert limits including approaches associated with channel numbers to is provided in Attachment D Ui 23/11/06 A 2007/70/II. szám A endix Annex 10 — Aeronautical Communications 3.6.5.6.1 Category I precision approach alert limits The alert limits are defined in Tables B-68 and B-69. For aircraft positions at which the lateral deviation exceeds twice the deviation at which full-scale lateral deflection of a course deviation indicator is achieved, or vertical deviation exceeds twice the deviation at which full-scale fly-down deflection of a course deviation indicator is achieved, both the lateral and vertical alert limits are set to the maximum values given in the tables. 3.6.5.6.2 AP alert limits. The alert limits are equal to the FASLAL and FASVAL for approaches with channel in the range of 20 001 to 39 999. For approaches with channel numbers in the range 40 000 to 99 999, the alert mits are stored in the on-board database. 3.6.5.7 Channel number Each GBAS approach transmitted from the ground subsystem is associated with a channel number in the range of 20 001 to 39 999. If provided, the GBAS positioning service is associated with a separate channel number in the range of 20 001 to 39 999. The channel number is given by: Channel number 20 000 40(F 108.0) 411(S) where F the data broadcast frequency (MHz) S RPDS or RSDS DS the reference station data selector for the GBAS ground subsystem (as defined in 3.6.4.3.1) k 2 of Type 2 message (as defined in 3.6.4.3.2.1), only RSDS are sed. able Category lateral alert limit Horizontal distance of aircraft position from the LTP/FTP as translated along the final approach path (metres) Lateral alert limit (metres) numbers li and RPDS the reference path data selector for the FAS data block (as defined in 3.6.4.5.1) RS For channel numbers transmitted in the additional data bloc u 291 D  873 FASLAL 873 D  7 500 0.0044D (m) FASLAL 3.85 D 7 500 FASLAL 29.15 able Category ertical alert limit Height above LTP/FTP of aircraft position translated onto the final approach path (feet) Vertical alert limit (metres) 100 H  200 FASVAL 200 H  1 340 0.02925H (ft) FASVAL 5.85 H 1 340 FASVAL 33.35 A 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I Note hen the FAS is not broadcast for an AP the AS approach is associated with a channel number in the range to Note uidance material concerning channel number selection is provided in Attachment D 3.6.5.8 EP EMERIS ERR R P SITI N UND Note Ephemeris error position bounds are computed only for core satellite constellation ranging sources used in the position s d not for other types of ran sources (S r pseudolites) e not subject to undetecte ever the calculation of these positio nformation from all ranging sources used in th 3.6.5.8.1 Category I precision approach and AP The vertical and lateral ephemeris error position bounds are defined as: VEB MAX VEBj j LEB MAX LEBj j The vertical and lateral e osition bound or the jth core stellation rang ng sour used in the position solution are given by: olution (j index) an ging s AS satellites o n b e i that ar d ephemeris failures ow ounds us e position solution (i index) phemeris error p s f satellite con i ce N j j air j md_e,j i VEB s_vert x K s_  ¦ i i vert uV P N j j air j md_e,j i i i LEB s_lat x P K s_lat  ¦ uV where: s_vert ined in 3.6.5.5.1.1 s_lati or j is defined in 3.6.5.5.1.1 xair 3.6.5.4 N ging sources used in the pos solution ıi Pj s decorrelation paramet for the jth ranging Kmd_e,j d detection multiplier for Category I precision approach and APV associated he jth ranging rce (Kmd_e,GPS or Kmd_e,GLONASS) 3. ervice. The horizontal ep positio efined as: HEB M HEBj The hor bound for the jth e satellite con nging source u e position solution i or j is def is defined in is the number of ran ition is defined in 3.6.5.5.1.1 st ephemeri is the broadca er source is the broadcast ephemeris misse ellite constellation for t with the sat sou 6.5.8.2 AS positioning s hemeris error n bound is d AX j izontal ephemeris error position cor stellation ra sed in th is given by: d j horz,j airPj md_e_POS major HEB s x K  23/11/06 A 2007/70/II. szám A endix Annex 10 — Aeronautical Communications where: is as defined in 3.6.5.5.2. sy,j is as defined in 3.6.5.5.2 xair is defined in 3.6.5.4 Pj broadcast ephemeris decorrelation para he jth ranging source Kmd_e_P is the broadcast ephemeris missed detection m lier for the GBAS positioning service asso iated with the r the jth ranging source (K POS,GPS or Kmd_ NASS) dmajor 3.6.6 M ES Each l be coded in accordance with th rresponding m defined in Tabl -70 through B-73. N age type structure is defined in 3.6.7 NON-A RAFT ELEMENT 3.6.7.1 PERF RMANCE 3.6.7. 3.6.7.1. S) (1 sigma ound subsys bution to the correct pseudo-range accuracy fo tes shall be: horz,j s xj yj s s  sx,j .1 is the meter for t OS satellite constellation fo ultip c md_e_ e_POS,GLO is as defined in 3.6.5.5.2.1 ESSAGE TABL GBAS message shal e co essage format es B ote Mess IRC S 1.1 Accuracy 1.1 The root-mean-square (RM ) of gr the tem contri ed r GPS and GLONASS satelli n / pr _ gnd (a a e ) RMS (a ) M T T  d  where M the number of GNSS reference s, as indic pe 2 message r (3.6.4.3), or, when this parameter is coded to indicate “not applicab e value of M is defi ed as 1; n nth ranging source; șn elevation angle for the nth ranging s ce; and a0, a1, eters defined in Tables B-74 and B-75 for eac defined ground acc designators (GADs). Note T racy re uirement is determined by the AD letter and the number of installed referen Note T to the corrected pseudo range error specified by the curves defined in Tables and S satellites do not include aircraft noise and aircraft multipath receiver ated in the Ty paramete le”, th n our a2, and ș0 param h e of th uracy he AS ground subsystem accu ce receivers he ground subsystem contribution and the contribution to the S A A 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I able ype 1 pseudo range corrections message Data content Bits used Range of values Resolution Modified -count 0 to 1 199.9 s 0.1 s Additional message flag 0 to 3 Number of measurements (N) 0 to 18 Measurement ty Ephemeris decorrelation parameter (P) 0 to 1.275 10 m/m 10 6 m/m s CRC ailability duration ent blocks rce ID C) .6 0.01 on (RRC) s 0.001 /s ıpr_gnd 0 t 0.0 0.0 0.05 0.05 0.0 pe 0 to 7 Ephemeri Source av — 0 to 2 540 s — 10 s For N measurem anging sou 1 t R o 25 Issue of data (IOD) ion (PR 0 to 255 27 7 m Pseudo-range correct ti m Range rate correc 32.767 m/ o m m 5.08 2 m B1 6.35 m 5 m B2 6.35 m 6. m B3 35 m m B4 6.35 m 5 m 0A ype 101 R pseudo range co tions message Data content Bits used Range of values Resolution able AS rrec Modified -count 0 to 1 199.9 s 0.1 s Additional message fla Number of measurements (N) 0 to 18 Measurement 0 to 7 Ephemeris decorrelation parameter (P) 0 to 1.275 10 3 m/m 6 m/m Ephemeris CRC — — Source availability ration 0 s 0 s Number of B param rs 0 or 4 — Spare — — For N measurement locks Ranging source ID 1 to 255 Issue of data (IOD) 0 to 255 Pseudo-range correction (PRC) 327.67 m 0.01 m Range rate corre 0.001 m/s ıpr_gnd 0.2 m B parameter block (if provided) B1 25.4 m B2 25.4 m B3 25.4 m B4 25.4 m g 0 to 3 type du 0 to 254 ete b ction (RRC) 327.67 m/s 0 to 50.8 m 0.2 m 0.2 m 0.2 m 0.2 m 23/11/06 A 2007/70/II. szám A endix Annex 10 — Aeronautical Communications able ype 2 AS related data message Data content Bits used Range of values Resolution GBAS reference receivers 2 to 4 — Ground accuracy designator letter — — Spare — — GBAS continuity/integrity designator 0 to 7 re — — ıvert_iono_gradient 0 to 25.5 10 6 m/m 0.1 10 6 m/m 16 to 781 Scale height 0 to 25 500 m 100 m Latitude 90.0 0.0005 arcsec Longitude 180.0 0.0005 arcsec GBAS reference point height 83 886.07 m 0.01 m 0 to 48 Maximum use distance (Dmax) 2 to 510 km 2 km Kmd_e_POS,GPS 0 to 12.75 0.05 Kmd_e,GPS 0 to 12.75 0.05 Local magnetic variation 0.25 Spa Refractivity index Refractivity uncertainty 0 to 2 Additional data block 1 (if provided) Reference station data selector Kmd_e_POS,GLONASS 0 to 12.75 0.05 Kmd_e,GLONASS 0 to 12.75 0.05 Additional data block 2 (if provided) Additional data block length 2 to 255 Additional data block number 2 to 255 Additional data parameters Variable — — able ype FAS data message Data content Bits used Range of values Resolution For N data sets Data set length 2 to 212 1 byte FAS data block — — FAS vertical alert limit/approach status

Source: https://magyarkozlony.hu/hivatalos-lapok/4c6310a937d14bac566ee9c9d944896656c292dd/dokumentumok/5a6ac3c6db12e692ae41096677ad5f072d2cc9f3/letoltes