Head-up Guidance & Vision Technologies Enabling Safer and More Efficient Airline Operations

Similar documents
Economics of Safety Using Situational Awareness Tools

OLM FBW 2006 Toulouse September Head Up Display

Operational Benefits, Affordability and Availability

TERMS OF REFERENCE (Revision 9) Special Committee (SC) 213 Enhanced Flight Vision Systems/Synthetic Vision Systems

HEAD-UP DISPLAY (HUD), EQUIVALENT DISPLAYS AND VISION SYSTEMS

PRO LINE FUSION INTEGRATED AVIONICS SYSTEM. Pro Line Fusion on Gulfstream G280: Your direct path to see and access more.

IATA Air Carrier Self Audit Checklist Analysis Questionnaire

Available Technologies. Asia / Pacific Regional Runway Safety Seminar Session 4

Available Technologies. Session 4 Presentation 1

ILS APPROACH WITH B737/A320

OPERATIONS CIRCULAR 01/2012. Subject: HEAD-UP DISPLAYS (HUD) AND ENHANCED VISION SYSTEMS (EVS)

Runway Excursion 2018 projects ALTA 2018

Pro Line Fusion integrated avionics system. Pro Line Fusion on Embraer Legacy 450 and 500: Business-jet technology designed with tomorrow in mind.

Agenda Item 5: Group Discussion How Could We Prevent Runway Excursions (Risks and Lessons Learned)

March 2016 Safety Meeting

Boeing s goal is gateto-gate. crew awareness that promotes safety and efficiency.

Runway Situation Awareness Tools Marisa Jenkins

NBAA Safety Committee Airports Group October 2015

Fly at the speed of ingenuity on your Learjet 85

Boeing 787 Dreamliner Flight Deck Safety, Comfort, Efficiency

Reducing The Risk of Runway Excursions. Jim Burin Director of Technical Programs

FLIGHT OPERATIONS PANEL

TAKEOFF SAFETY ISSUE 2-11/2001. Flight Operations Support & Line Assistance

Jet Transport Airplane Performance - Briefing For Business Aviation Pilots & Operators

Preventing Runway Excursions. Technical solutions From the Design and Manufacturing Sector

Air Navigation Bureau ICAO Headquarters, Montreal

Introduction to ROPS. Runway Overrun Prevention System. Presented by: Jerome JOURNADE ROPS Technical Manager

APPENDIX X: RUNWAY LENGTH ANALYSIS

ONE-ENGINE INOPERATIVE FLIGHT

A Human Factors Approach to Preventing Tail Strikes. Captain Vern Jeremica Senior Safety Pilot Boeing Commercial Airplanes May 2004

FlyRealHUDs Very Brief User s Manual

Instrument Proficiency Check Flight Record

Safety Enhancement SE ASA Design Virtual Day-VMC Displays

F1 Rocket. Recurrent Training Program

Decisions on which type of approach to use vary with each airline, and sometimes even for each flight. aero quarterly qtr_02 10

HARD. Preventing. Nosegear Touchdowns

Advisory Circular. Regulations for Terrain Awareness Warning System

All-Weather Operations Training Programme

CDA Continuous Descent Approach

PACIFIC AEROSTAR L.L.C.

PRO LINE FUSION UPGRADE FOR YOUR CITATION CJ3. Your all-in-one approach for airspace modernization and situational awareness.

EXPERIMENTAL STUDY OF VERTICAL FLIGHT PATH MODE AWARENESS. Eric N. Johnson & Amy R. Pritchett

Advisory Circular. U.S. Department of Transportation Federal Aviation Administration

Rethink Convention. LEGACY 450

PRO LINE FUSION ADVANCED AVIONICS. Easier, more predictable flight. Scaled to your aircraft.

June 9th, 2011 Runway Excursions at Landing The n 1 Global Air Safety Issue Can We Reduce this Risk Through Innovative Avionics?

BUILDING LOCAL RUNWAY EXCURSION ACTION PLAN UNSTABILISED APPROACHES. Lisbon, 4 th Dec 2013

FUEL MANAGEMENT FOR COMMERCIAL TRANSPORT

Surveillance and Broadcast Services

USE OF RADAR IN THE APPROACH CONTROL SERVICE

Dive-and-Drive Dangers

SAFETY HIGHLIGHTS CESSNA CITATION AOPA AIR SAFETY INSTITUTE 1 SAFETY HIGHLIGHTS CESSNA CITATION

Landing on Slippery Runways. BOEING is a trademark of Boeing Management Company. Copyright 2007 Boeing. All rights reserved.

Private Pilot Flight Training

Single Engine Instrument Training Record I PREFLIGHT PREPARATION WEATHER INFORMATION weather reports and forecasts. pilot and radar reports.

Flight Operations in Low Visibility Conditions

Approach-and-Landing Briefing Note Response to GPWS Pull-Up Maneuver Training

Research on Controlled Flight Into Terrain Risk Analysis Based on Bow-tie Model and WQAR Data

This page intentionally left blank.

Don-Jacques OULD FERHAT VP Airspace and Airlines Services. Airbus. PBN Safety programs

RNP AR APCH Approvals: An Operator s Perspective

Advanced Transition Training

Quiet Climb. 26 AERO First-Quarter 2003 January

Taking your Pro Line 21 King Air into NextGen airspace. Pro Line 21 INTEGRATED AVIONICS SYSTEM FOR KING AIR

Taking your Pro Line 21 Hawker into NextGen airspace. Pro Line 21 INTEGRATED AVIONICS SYSTEM FOR HAWKER

RNP In Daily Operations

EUROCAE ED-250: ROAAS MOPS

QUIETER OPERATIONS A GUIDE FOR PILOTS AND CONTROLLERS

NOISE ABATEMENT PROCEDURES

Avionics Mandates (Part 7):

SECURITY OVERSIGHT AGENCY June 2017 ALL WEATHER (CAT II, CAT III AND LOW VISIBILITY) OPERATIONS

1. BASIC PRINCIPLES OF AOA

CESSNA SECTION 5 PERFORMANCE

Civil Air Patrol. National Flight Academy Powered Middle East Region. Flight Instruction Syllabus

AFI Flight Operations Safety Awareness Seminar (FOSAS)

KSFO RNAV TO GLS DEMONSTRATION

Rethink Convention. LEGACY 500

VFR into IMC. Safety Syllabus

Weight and Balance User Guide

Scenario 1 - VFR Flight -KBUY Cessna SEP/G1000 Scenario Based Training Objective: Prerequisites: PT Preparation: Briefing Items: Safety: Preflight:

Beijing, 18 h of September 2014 Pierre BACHELIER Head of ATM Programme. Cockpit Initiatives. ATC Global 2014

Advisory Circular. Flight Deck Automation Policy and Manual Flying in Operations and Training


Operators may need to retrofit their airplanes to ensure existing fleets are properly equipped for RNP operations. aero quarterly qtr_04 11

Runway Safety Programme Global Runway Safety Action Plan

FALCON SERVICE ADVISORY

OPERATIONAL USE OF ANGLE OF ATTACK ON MODERN COMMERCIAL JET AIRPLANES

LESSON PLAN Introduction (3 minutes)

USE OF LANDING CHARTS [B737]

airplane rating, holds a multiengine land rating, and meets the recent flight experience of 14CFR for TO & LDGS in the preceding 90 days.

airplane rating, holds a multiengine land rating, and meets the recent flight experience of 14CFR for TO & LDGS in the preceding 90 days.

LOFT A/B-90 SIM PRE/POST

AERONAUTICAL SURVEYS & INSTRUMENT FLIGHT PROCEDURES

Navigation - Runways. Chap 2, Nolan

Helicopter Performance. Performance Class 1. Jim Lyons

Safety Syllabus. VFR into IMC

Weather Information for Pilots

AERODROME OPERATING MINIMA

POST-IMPLEMENTATION COMMUNITY IMPACT REVIEW

Transcription:

Head-up Guidance & Vision Technologies Enabling Safer and More Efficient Airline Operations March, 2017 2017 Rockwell 2017 Collins. Rockwell Collins.

Agenda > HGS Introduction > HGS Value Safety & Economics > Vision Systems a view to the future > Worldwide Adoption 2

What is HGS? A Quick Introduction HGS = Head-up Guidance System Rockwell Collins Head-Up Display exclusive for aviation First introduced in commercial aviation in the mid-1980 s Presents critical flight information and guidance as pilots look outside Flight path Energy Altitude Patented guidance Unique flight safety features 3

Aviation Safety Considerations 3% of approaches worldwide remain unstable Flight Safety Foundation Runway excursions, tailstrikes, and hard landings are costly, yet preventable Industry recognizes pilot manual flying skills are weakening FAA SAFO Go-Around execution is still are not to the level of proficiency to meet operational and regulatory compliance FAA SAFO What does one major tailstrike cost? 4

Safety Benefits of HGS Technology HGS would have highly likely or likely prevented Takeoff & Landing Loss of Control 69% 57% 5

HGS Provides Optimum Go-Around Guidance and Precision Key Go-Around symbology Flight Path, Boresight, Pitch Target, Energy Caret, Airspeed/Speed Error Tape, at fifty feet transition to Flight Director Cue 6

Typical Nighttime Approach at Unimproved Airport 7

Typical Nighttime Approach at Unimproved Airport w/hgs 8

HGS/HUD Optimizes Stabilized Approach - Flight Path Group The flight path group of symbols are the heart of creating a stabilized approach. Boresight FPV Flight Path Vector Inertia Caret Speed Error Tape By using the inertially derived flight path, the HGS symbology shows flight path information to the pilot that is conformal with the real world. In other words, what the pilot sees in the HGS is what they can expect to see outside the aircraft; the pilot s eyes will already be focused on the landing runway aim point before the runway is in view. 9

HGS Rollout Information The HGS provides consistent speed, deceleration, runway remaining information to the pilot. In addition the deceleration brake index markings correlate to the autobrake settings and when used with runway remaining provides the pilot with real time braking efficiency information. Once on the ground - Key information for stopping capability to avoid runway excursion 10

HGS Provides Means to Avoid Runway Excursion Risks associated with runway overruns during landing phase of flight Hazards associated with runway overruns (EASA, FAA, NTSB) Non-stabilized approach Too high on approach (steep) Tailwind Incorrect decision to land Excess airspeed (high touchdown speed) Landing beyond touchdown point (long landing) Failure to assess required landing distance Wet/contaminated runway Late/incorrect use of brakes Late/incorrect use of reverse thrust Aquaplaning 11

FAA AC 91-79 (Stabilized Approach) Landing Configuration Landing gear down Landing flaps selected Trim set Fuel balanced Landing checklist completed Stabilized on Profile IMC at 1000 feet above TDZE VMC at 500 feet above TDZE Proper landing configuration Correct lateral track Correct vertical track Optimum 3 degree glide path (greater than 3 degrees are special cases ) Airspeed within acceptable range Descent Rate Optimum 500 to 700 fpm Not exceed 1000 fpm Indicated Airspeed Not more than Vref+5 with adjustment for wind and other factors Never less than Vref Go-Around should be executed at any time approach is determined to be unstable 12

FAA AC 91-79 (Landing Distance Calculations) 13

Increased Stopping Awareness Inertia Caret indicates the deceleration rate of the airplane Units Equivalent to Autobrake Feet Remaining (or Meters) 500 ft increments using GPS Graphical Brake Scaling (predictive stopping indication) 14

HGS 4000 and HGS 6000 Dual Configuration 15

Additional Safety Benefits Tailstrike Avoidance Guidance during emergencies: Engine out, windshear, unusual attitude Stabilized approaches, preventing runway excursions Dynamic runway remaining information Consistent landing position 16

Economics of HGS - Airlines Civil Aviation Authorities allow exclusive operations for HGS Examples: Flight Phase Runway ILS Airport Visibility Aircraft without HGS Aircraft with HGS Landing Category I 600m Can Land Can Land Landing Category I 350m Cannot Land Can Land Takeoff Category I 200m Cannot Takeoff Can Takeoff With HGS fewer flights are disrupted, resulting in: Lower fuel costs Fewer delays/cancellations Increased customer loyalty/revenue 17

A view to the future VISION SYSTEMS

Enhanced Flight Vision System (EFVS) Enhanced Vision Sensor generates a real-world video image of scene ahead displayed on a HUD System utilizes at least one sensor, usually positioned in the airplane radome 19

EVS-3000 Flight Test Video 20

Current Flight Operational Capability Gaps How do you get passengers here at night? What happens if you can land, but you cannot taxi? Runway incursions remain a problem.

EFVS Value Proposition Taxi / land / takeoff in low visibility at any airport Ground equipment not required Prevent dangerous operations resulting from losing awareness Collisions with vehicles, people, animals, etc Runway incursions Potential to open airports for nighttime operations Regional airports that lack runway/taxiway lights Increase fleet utilization rates for regional aircraft Maintain flight schedules in smoke/haze/dust and some fog 22

Synthetic Vision System (SVS) on HGS Computer generated world view from pilot s perspective SVS database consists of 3 layers Terrain Obstacle Airports & Runways 23

Head-up Combined Vision 24

ADOPTION WORLDWIDE

Aircraft Manufacturers Support HGS Technology Head-Up Displays are now offered on all next generation aircraft, either as baseline or option Rockwell Collins HGS is the most trusted and widely adopted Head-Up Display in aviation Over 7,000 HGS delivered Selected by the worlds most recognized aircraft manufacturers 26

Aviation Authorities Support HGS Technology Civil aviation authorities recognize HGS operational and safety impacts Exclusive operational capabilities granted for HGS operators China will require all in-country aircraft to equip with HUD by 2025 China HUD Roadmap 2015 2020 2025 HUD Equipage Requirement 10% 50% 100% Additional credits for HGS, EFVS, SVS are in development 27

Airline Operators of HGS Africa Americas Asia/Pacific Europe Middle East 28

United States B737 HGS Equipage 78% U.S. based B737 equipped with HGS 29

In Conclusion Operating environment and infrastructure in Southeast Asia warrant broader use of Head-Up Displays HGS allows airlines to run more economically by: Reducing the number of flight disruptions Maximizing safety margins Saving unnecessary maintenance costs Vision technologies offer a significant operational opportunity for airlines HGS & Vision Systems are a necessary consideration 30