AIRBUS AND APV LVP APPROACHES
December 30, 2016 | Author: IYIBIRI | Category: N/A
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Description
ICAO LVP&APV workshop – 9-11 June 2009
Presented by:
Edith PABON-ALQUIER Airbus Flight Operations Support & Services
Airbus aircraft capacities to support APV
Content
ÒLNAV/VNAV – Baro VNAV ÒRNP AR APCH
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
ÒAirbus FMS Landing System - FLS ÒSBAS – Satellite Landing System ÒConclusion
ICAO LVP&APV workshop
June 09
Page 2
LNAV/VNAV – Baro-VNAV • During LNAV/VNAV, Baro-VNAV, the aircraft system uses barometric altitude to compare the vertical position of the aircraft with vertical flight path computed by the FMS, also using baro-referenced altitudes.
• The fly-by-wire Airbus aircraft are equipped with integrated
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
LNAV/VNAV systems with accurate source of barometric altitude.
• Airbus fly-by-wire aircraft systems have been certified by EASA to conduct Baro-VNAV approaches down to a MDA/H of minimum 250ft.
ICAO LVP&APV workshop
June 09
Page 3
Content
ÒLNAV/VNAV – RNP APCH ÒRNP AR APCH
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
ÒAirbus FMS Landing System - FLS ÒSBAS – Satellite Landing System ÒConclusion
ICAO LVP&APV workshop
June 09
Page 4
Airbus Basic RNP Capabilities – RNP APCH • Basic certification was demonstrated by reference to the MASPS DO-236 / ED-75 • Achieved with AP or FD ON in GPS PRIMARY mode Approach
Terminal
En-route
Airbus Certified Capability
RNP 0.3
RNP 0.51
RNP 1(2)
Required Capability
RNP 0.3
RNP 1
RNP 2(4)
•RNP 0.3 applicable to straight in approaches designed under ICAO © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
PANS OPS or FAA TERPS criteria.
•All Airbus equipped with FMS and GPS are capable to fly RNP APCH as per ICAO PBN manual.
•DH as low as 250 ft with FINAL APP mode (LNAV/VNAV ) guidance. Note: This certification was not intended for RNP AR (or SAAAR) operations, including RNP AR APCH of ICAO PBN manual. ICAO LVP&APV workshop
June 09
Page 5
RNP AR Concept RNP RNPAR ARConcept Concept • A procedure is RNP AR if one of the following characteristic is present: Reduced obstacle protections, at 2xRNP, without buffers
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
2 x RNP
VEB
RNP values lower than 0.3 in approach
Curved flight path below FAF (RF legs)
ICAO LVP&APV workshop
June 09
Page 6
RNP AR Certification standards In some cases, obstacle may be as close as 2xRNP. Need to demonstrate a Target Level of Safety of 10-7/approach Including the effect of system failures
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Existing airborne systems are not capable to meet this objective alone Operational mitigations are required to achieve the overall safety objectives (FOSA) ICAO LVP&APV workshop
June 09
Page 7
RNP AR Certification standards FAA: Rely on Flight Operational Safety Assessment (FOSA) Engine failure evaluation in ops context A/C to be maintained within 2xRNP
EASA certification requirements: © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
• Engine failure or probable system failures (>10-5/procedure): A/C to be maintained within 1xRNP
• Remote system failures (10-5 to 10-7/procedure) : A/C to be maintained within 2xRNP
• Safe extraction for failures below 10-7
ICAO LVP&APV workshop
June 09
Page 8
RNP AR below 0.3 Certification
Lateral Deviation scale Automatic NAV re-engagement
RNP AR EASA © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Certification Requirements
at GA initiation
Triple click upon loss of FINAL APP or NAV EGPWS with GPS position and peaks mode
ICAO LVP&APV workshop
June 09
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RNP AR below 0.3 Certification Lateral Deviation & Improved XTRK error resolution SPEED
FINAL APP MDA 250
AP1 1FD2 A/THR
V/DEV
Improved XTK Error resolution on ND: • 2 digits after the dot
• When 0.02 ≤ XTK ≤ 0.29
RNP L/DEV
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
ON
• RNP Push Button enables the LATDEV New Lateral Deviation Indication:
• L/DEV displayed on PFD • Position of the computed flight plan • Full scale: 2 dots = +/- 0.2 NM • Same symbol as the V/DEV ICAO LVP&APV workshop
•
display. With latest standards of equipment, the P/B is no more required:
The L/DEV is automatically displayed when needed June 09
Page 10
Certification for RNP AR below 0.3 A318/A319/A320/A321 A318/A319/A320/A321 aircraft aircraft ntly e r r Cu
Approach
Departure
(AP on)
Missed Approach (AP on)
RNP 0.1 (normal)
RNP 0.17 (normal)
RNP 0.17 (normal)
(AP on)
RNP 0.24 (non normal)
New
Approach
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
(AP on)
Missed Approach (AP on)
Departure (AP on)
RNP 0.1 (normal) and RNP 0.2 (non normal) Availability planned Q4 2009
Requires Specific Set of Equipment Package
ICAO LVP&APV workshop
June 09
Page 11
Certification for RNP AR below 0.3 A330-200/-300 A330-200/-300 aircraft aircraft ntly Approach e r r Cu (AP on)
Missed Approach (AP on)
RNP 0.1 (normal) RNP 0.3 (normal)
Departure (AP on)
RNP 0.1 (normal)
RNP 0.3 (non normal)
New
Approach
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
(AP on)
Missed Approach (AP on)
Departure (AP on)
RNP 0.1 (Normal) and RNP 0.2y (non normal) Availability planned Q2 2010
Requires Specific Set of Equipment Package
ICAO LVP&APV workshop
June 09
Page 12
Certification for RNP AR below 0.3 A340-500/-600 A340-500/-600 aircraft aircraft
Approach (AP on)
Missed Approach (AP on)
RNP 0.1 (normal) RNP 0.3 (normal)
Departure (AP on)
RNP 0.1 (normal)
RNP 0.2
RNP 0.3
RNP 0.2
(non normal)
(non normal)
(non normal)
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Availability planned Q2 2009
Requires Specific Set of Equipment Package
ICAO LVP&APV workshop
June 09
Page 13
The RNP AR limited to 0.3. RNP AR procedures are not all equivalent in terms of exposure:
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Flight
around obstacles Noise abatement, Track miles saving, Traffic management, ….
ICAO LVP&APV workshop
June 09
Page 14
The RNP AR limited to 0.3. On OnA318/A319/A320/A321 A318/A319/A320/A321 &&A330/A340-600/A340-500 A330/A340-600/A340-500
w e N
Approach
Missed Approach (AP on)
(AP on)
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
RNP 0.3 (normal &
(AP on)
non norm)
•
Availability end of the year 2009, or early 2010,
•
No LAT DEV required.
•
reduced set of equipment
ICAO LVP&APV workshop
Departure
June 09
Page 15
Content
ÒLNAV/VNAV – RNP APCH ÒRNP AR APCH
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
ÒAirbus FMS Landing System - FLS ÒSBAS – Satellite Landing System ÒConclusion
ICAO LVP&APV workshop
June 09
Page 16
FMS Landing System (FLS) • Airbus has decided to modify the current cockpit design for Non Precision Approach operational procedures to provide similar interface for Non Precision Approach as for Precision Approach (ILS Look alike)
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
• This new design allows conducting existing non precision approaches (VOR, VOR/DME, NDB, NDB/DME, GPS) in the same manner as Precision Approach (ILS/GLS) with similar display, guidance & warnings. •This function is autonomous and does not require any additional information from the ground. •Applies to straight in approach flight path.
FLS is a new way to fly NPA – not a new type of approach ICAO LVP&APV workshop
June 09
Page 17
FLS Principle • Based on database stored data, an FLS approach beam is defined. Then, lateral and vertical deviations between the FLS beam and the computed aircraft position are computed by the MMR and used for guidance and display to the pilot.
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Anchor point
The FLS virtual beam is defined by: • Anchor Point • Course • Slope
FLS beam
FAF
FLS beam FAF Anchor Point
Course
Slope
Anchor Point ICAO LVP&APV workshop
June 09
Page 18
FLS display
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
6
5
1) Pseudo LOC scale & index 2) Pseudo G/S scale & index 3) Course pointer 4) FLS beam definition Anchor Point identification Slope Distance to RWY threshold 5) Approach capability 6) AP/FD guidance modes
2
4 ICAO LVP&APV workshop
3 1 June 09
Page 19
FLS Benefits • Stabilized approach Enhanced
safety operation:
– 80% of approach accidents occur on non stabilized approaches FLS
available all over the world:
– non precision approaches published on any airport in the world
• ILS Look alike © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
HMI
close to precision approaches Reuse of ILS pilot skills , reduction in training needs. Use of ILS guidance laws in Flight Guidance: same behavior as precision approaches Temperature compensated
ICAO LVP&APV workshop
June 09
Page 20
FLS policy and schedule • FLS is a Multi Programme Project – Will be certified on all current Airbus fly-by-wire aircraft Basic
on A380 and A350
Optional
on SA and LR programs
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
• Certification schedule: A380:
At Entry into service A320 family: end 09 A330/A340 family: from 2010
ICAO LVP&APV workshop
June 09
Page 21
Content
ÒLNAV/VNAV – RNP APCH ÒRNP AR APCH
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
ÒAirbus FMS Landing System - FLS ÒSBAS – Satellite Landing System ÒConclusion
ICAO LVP&APV workshop
June 09
Page 22
Satellite Landing System Allows to fly RNAV (GNSS) approaches with vertical guidance down to 200ft without any xLS ground station First step: A350XWB
Future steps:
procedures: RNAV GNSS with LPV minima (down to 200’) Technical enabler: GPS+SBAS Coverage: multi regional Cockpit integration (HMI, NDB, ..)
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Targeted
GPS L1 SBAS L1 GALILEO L1/E5 GPS L1 GPS L1 WAAS L1
2003 ICAO LVP&APV workshop
Technical
enablers: all new GNSS means capable of LPV200’ Coverage: worldwide
GPS L1/L5 SBAS L1/L5 GALILEO SOL L1/L5
GPS L1 W. / E. L1 WAAS/ EGNOS L1 GAGAN/ MSAS L1
2009
2011
GPS L1/L1C/L5 SBAS L1/L5 GALILEO SOL L1/L5
2013
A350XWB
2018
2023 June 09
Page 23
Main benefits No need for local ground station
Provide geometrical vertical guidance
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Give access to RNAV GNSS with LPV minima down to 200’
SBAS
ICAO LVP&APV workshop
June 09
Page 24
Experimental flight tests • SBAS flight tests performed on A380 With
a modified MMR, In an experimental configuration with SBAS on one side and GBAS on the other side To mature function for A350 and collect SBAS data
• Project launched for A350 to provide SBAS Landing © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
System (SLS) with capability to perform LPV-200 approaches (where available)
• Currently no plans to introduce SLS for existing programmes
ICAO LVP&APV workshop
June 09
Page 25
Content
ÒLNAV/VNAV – RNP APCH ÒRNP AR APCH
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
ÒAirbus FMS Landing System - FLS ÒSBAS – Satellite Landing System ÒConclusion
ICAO LVP&APV workshop
June 09
Page 26
Conclusion 9Satellite based systems and RNP operations foreseen as the final successor to ground based aids. 9Airbus supports the development of new landing systems in line with operator requirements.
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
¾MLS, FLS, SBAS (SLS) ¾MMR is the key to enable all approaches (precision and non precision) to be flown the same way.
9RNP AR : most of the fly by wire a/c are RNP AR capable. ¾Airbus has already met more stringent EASA requirements ¾Reduced operational demonstration for airlines ¾Higher confidence from national authorities
ICAO LVP&APV workshop
June 09
Page 27
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