Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 3170

c) a failure of eying 3 Re uirements for t e lobal a igation Satellite System SS 3.7.1 Definitions Aircra t ased au mentation s stem (A A ) An augmentation system that augments and/or integrates the information obtained from the other GNSS elements with information available on board the aircraft. Alert An indication provided to other aircraft systems or annunciation to the pilot to identify that an operating parameter of a navigation system is out of tolerance. Alert limit For a given parameter measurement, the error tolerance not to be exceeded without issuing an alert. C annel o standard accurac (C A) The specified level of positioning, velocity and timing accuracy that is available to any GLONASS user on a continuous, worldwide basis. Core satellite constellation(s) The core satellite constellations are GPS and GLONASS. lo al navi ation satellite s stem ( ) A worldwide position and time determination system that includes one or more satellite constellations, aircraft receivers and system integrity monitoring, augmented as necessary to support the required navigation performance for the intended operation. lo al navi ation satellite s stem ( A ) The satellite navigation system operated by the Russian Federation. lo al ositionin s stem ( The satellite navigation system operated by the United States 2007/70/II. szám C a ter Annex 10 — Aeronautical Communications 23/11/06 osition error The difference between the true position and the position determined by the GNSS receiver. round ased au mentation s stem ( A ) An augmentation system in which the user receives augmentation information directly from a ground-based transmitter. round ased re ional au mentation s stem ( A ) An augmentation system in which the user receives augmentation information directly from one of a group of ground-based transmitters covering a region. Inte rit A measure of the trust that can be placed in the correctness of the information supplied by the total system. Integrity includes the ability of a system to provide timely and valid warnings to the user (alerts). seudo ran e The difference between the time of transmission by a satellite and reception by a GNSS receiver multiplied by the speed of light in a vacuum, including bias due to the difference between a GNSS receiver and satellite time reference. atellite ased au mentation s stem ( A ) A wide coverage augmentation system in which the user receives augmentation information from a satellite-based transmitter. tandard ositionin service ( ) The specified level of positioning, velocity and timing accuracy that is available to any global positioning system (GPS) user on a continuous, worldwide basis. ime to alert The maximum allowable time elapsed from the onset of the navigation system being out of tolerance until the equipment enunciates the alert. 3.7.2 General 3.7.2.1 Functions 3.7.2.1.1 The GNSS shall provide position and time data to the aircraft. Note These data are derived from pseudo range measurements between an aircraft e uipped with a NSS receiver and various signal sources on satellites or on the ground 3.7.2.2 NSS elements 3.7.2.2.1 The GNSS navigation service shall be provided using various combinations of the following elements installed on the ground, on satellites and/or on board the aircraft:

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