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C ENTRE D'ETUDES DE LA NAVIGATION AERIENNE ASAS-TN, 2nd workshop - Malmö 6 ~ 8 october 2003page 1 Electronic separation Clearance Enabling the Crossing of Traffic under Instrument meteorological Conditions
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C ENTRE D'ETUDES DE LA NAVIGATION AERIENNE ASAS-TN, 2nd workshop - Malmö 6 ~ 8 october 2003page 2 ECLECTIC: What is it? To assess operational feasibility and acceptability of ASAS Crossing Procedures (ACP) Procedures which allow the flight crew to provide separation with respect to one aircraft designated by ATC The controller remains responsible for separation of other aircraft Airborne separation Minima A CENA Project : prospective study for Package 2 European context : EEC, NUP II, MFF, MA-AFAS
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C ENTRE D'ETUDES DE LA NAVIGATION AERIENNE ASAS-TN, 2nd workshop - Malmö 6 ~ 8 october 2003page 3 ECLECTIC: How? First step A demonstrator running on PC unit Several scenarios of crossing Different crossing angles Different altitudes and speeds Different horizontal separation at CPA before ASAS manoeuvre Controller radar display Flight deck MMI example (CDTI + control unit) Automatic or manual initiation of ACP and piloting (through pseudo A/P) Further steps Experimentations with traffic simulator and real controllers Traffic scenarios with several aircraft
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C ENTRE D'ETUDES DE LA NAVIGATION AERIENNE ASAS-TN, 2nd workshop - Malmö 6 ~ 8 october 2003page 4 ECLECTIC: An example of ACP ASAS « lateral crossing procedure »: Aircraft cleared for ACP Crossed (« designated ») aircraft Manoeuvring envelope « Clear of Traffic » New « ACP » trajectory Initial planned trajectory New waypoints introduced by ASAS algorithms
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C ENTRE D'ETUDES DE LA NAVIGATION AERIENNE ASAS-TN, 2nd workshop - Malmö 6 ~ 8 october 2003page 5 Considerations & assumptions ACP considered as a « standard » procedure Proposed by ATC If impossible, flight crew will advise ATC immediately No monitoring by ATC ACP is considered as safe as today’s procedures Airborne separation value may be different from the radar one Radar separation minima are not the same everywhere The airborne value may depend on the equipment Contingency in case of « ASAS unavailability » The ACP abortion does not mean immediate risk of collision ATC should be able to recover ATC may use half vertical separation as a last resort ACAS
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C ENTRE D'ETUDES DE LA NAVIGATION AERIENNE ASAS-TN, 2nd workshop - Malmö 6 ~ 8 october 2003page 6 Scenarios Different crossing angles: « Head-on » « crossing » « Same route »
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C ENTRE D'ETUDES DE LA NAVIGATION AERIENNE ASAS-TN, 2nd workshop - Malmö 6 ~ 8 october 2003page 7 Different solutions Pass behind… Or in front
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C ENTRE D'ETUDES DE LA NAVIGATION AERIENNE ASAS-TN, 2nd workshop - Malmö 6 ~ 8 october 2003page 8 Issues The phraseology must remain simple and robust The « other aircraft » designation is still an open issue Unambiguous Must not generate confusion with traffic not involved The need to lock the navigation of the other aircraft and to advise it about the ASAS crossing, to be discussed End of procedure: At « Clear of Traffic », or After resuming navigation?
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C ENTRE D'ETUDES DE LA NAVIGATION AERIENNE ASAS-TN, 2nd workshop - Malmö 6 ~ 8 october 2003page 9 Example of phraseology Atc: ABC123, for ASAS separation, identify traffic Pil : Traffic identified, ABC123 Atc: ABC123, pass behind traffic, maintain airborne separation, report clear of traffic (or : resuming navigation) Pil :Passing behind traffic, maintaining airborne separation, ABC123 … ( the controller is NOT required to monitor the crossing) Pil : ABC123, clear of traffic (or: resuming navigation) Atc: ABC123, roger. * note : the unambiguous identification of the other aircraft is still an open issue, which may be solved through data-link communication
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C ENTRE D'ETUDES DE LA NAVIGATION AERIENNE ASAS-TN, 2nd workshop - Malmö 6 ~ 8 october 2003page 10 How does it work ? Traffic scenario Simplified aircraft simulator ASAS algorithm + parameters computes alternative routes for separation The aircraft is piloted in real time though A/P commands The HMI (ND) is for demo and experimentations purpose, not a proposal for implementation
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C ENTRE D'ETUDES DE LA NAVIGATION AERIENNE ASAS-TN, 2nd workshop - Malmö 6 ~ 8 october 2003page 11 Crossing at 120° angle (1/6) The other aircraft has been identified Its flight path is displayed (magenta track) Current distance between aircraft: 153NM (display range 320NM)
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C ENTRE D'ETUDES DE LA NAVIGATION AERIENNE ASAS-TN, 2nd workshop - Malmö 6 ~ 8 october 2003page 12 Crossing at 120° angle (2/6) The ASAS system has been switched on: an alternative route (with offset solution) is proposed to the pilot (yellow dotted line) (display range 160NM)
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C ENTRE D'ETUDES DE LA NAVIGATION AERIENNE ASAS-TN, 2nd workshop - Malmö 6 ~ 8 october 2003page 13 Crossing at 120° angle (3/6) The alternate route is activated : its colour is changed to green The separation is assured at the required value (here: 8NM) (display range 160NM)
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C ENTRE D'ETUDES DE LA NAVIGATION AERIENNE ASAS-TN, 2nd workshop - Malmö 6 ~ 8 october 2003page 14 Crossing at 120° angle (4/6) The aircraft is following the new route (display range 80NM)
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C ENTRE D'ETUDES DE LA NAVIGATION AERIENNE ASAS-TN, 2nd workshop - Malmö 6 ~ 8 october 2003page 15 Crossing at 120° angle (5/6) (display range 40NM)
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C ENTRE D'ETUDES DE LA NAVIGATION AERIENNE ASAS-TN, 2nd workshop - Malmö 6 ~ 8 october 2003page 16 Crossing at 120° angle (6/6) Aircraft have passed the CPA at (slightly less than) the required separation value… Own aircraft can resume its navigation (here, « direct to ») (display range 40NM)
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C ENTRE D'ETUDES DE LA NAVIGATION AERIENNE ASAS-TN, 2nd workshop - Malmö 6 ~ 8 october 2003page 17 First results of achieved separation Parameters: Offset solution Required separation value : 8NM Angle of deviation : 60° (crossings at 23°) 30° (crossings at other angles) Crossings : 23° : 60° : 120°: Head-on
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C ENTRE D'ETUDES DE LA NAVIGATION AERIENNE ASAS-TN, 2nd workshop - Malmö 6 ~ 8 october 2003page 18 Further work Other parameter values 5NM, 3NM as examples for separation Other angles of deviation « Pass in front » Other algorithms One waypoint solution Open angle of deviation Manoeuvring Envelope Simulations
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