Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 3458

b) the coordinates of n-satellite in P -90 coordinate system at an instant tb; n b x (t ),  n b y (t ),  n b z (t )  the velocity vector components of n-satellite in P -90 coordinate system at an instant tb; the acceleration components of n-satellite in n b x (t P -90 coordinate system at an instant t ),  n b y (t ),  n b z (t )  b, which are caused by effect of sun and moon; A 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I En al elapsed since the instant of its calculation (uploading) until the instant t for n-satellite; B the health flag. Values greater than 3 indicate the fact of malfunction of given satellite; P1 al between the current and previous value of the tb parameters in minutes as shown: Time interval between adjacent values of tb in minutes an indication of the “age” of the immediate information, i.e. a time interv b n a flag indicating the time interv P1 P2 lue of “0” indicates a 60-minute interval of service information transmit (t 2, 6, 10 ); P3 ithin a given frame. “1” corresponds to 5 satellites and “0” corresponds to 4 satellites; and ǻĲn in L2 sub-band and navigation RF signal transmitted in L1 sub-band by given satellite: ǻĲ t t where t , t are the equipment delays in L1 and L2 sub-bands respectively, expressed in units of time. he MSB shall be the sign bit. The chip “0” shall correspond the “ ” sign and the chip “1” shall correspond to the “ ” sign. time parameters Arrangements of the ephemeris and time parameters ithin a frame shall be as indicated in Table B-18. 3.2.1.3.4 Almanac parameters The almanac parameters shall be as follows: an index showing relation of this parameter with the almanac; MA n f the modification of nA-satellite: “00” indicates GLONASS satellite, and “01” indicates GLONASS-M satellite; the GLONASS time scale correction to UTC(SU) time. The correction Ĳ is given at the instant of day NA; NA . The correction Ĳc and other almanac data (almanac of orbits and almanac of phases) relate to this day number; the slot number occupied by n-satellite; A the channel number of a carrier frequency of nA-satellite (Table B-16); A the longitude of the first (within the NA-day) ascending node of nA-satellite orbit in P -90 coordinate system; tȜ A n the time of the first ascend a flag indicating whether the value of tb is odd or even. A value of “1” indicates a 30minute interval of service information transmit (tb 1, 3, 5 ), a va b a flag indicating the number of satellites for which an almanac is transmitted w the time difference between the navigation RF signal transmitted n f2 f1 f1 f2 3.2.1.3.2 Ephemeris and time parameters. The ephemeris and time parameters shall be as indicated in Table B-17. For the words for which numeric values may be positive or negative, t to 3.2.1.3.3 Arrangement of the ephemeris and w A an index o Ĳc c the calendar day number within the 4-year period beginning since the leap year A n H n Ȝ n ing node passage of nA-satellite within NA-day; 23/11/06 A 2007/70/II. szám A endix Annex 10 — Aeronautical Communications able 1 Ep emeris and time parameters Parameter of bits Sc r (LSB) Ef ra Number ale facto fective nge Units m ionless nless nds x (t (t ) x y

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