Flight Safety Research in Japan October 3, 2005 ICAS PC Meeting - - PowerPoint PPT Presentation

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Flight Safety Research in Japan October 3, 2005 ICAS PC Meeting - - PowerPoint PPT Presentation

Flight Safety Research in Japan October 3, 2005 ICAS PC Meeting Workshop, Mykonos, Greece Yoshikazu Miyazawa Air Safety Technology Center Japan Aerospace Exploration Agency (JAXA) Outline 1. Introduction 2. Cabin Safety Turbulence detection


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SLIDE 1

Flight Safety Research in Japan

October 3, 2005 ICAS PC Meeting Workshop, Mykonos, Greece Yoshikazu Miyazawa Air Safety Technology Center Japan Aerospace Exploration Agency (JAXA)

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SLIDE 2

Outline

  • 1. Introduction
  • 2. Cabin Safety

Turbulence detection laser radar (lidar) development

  • 3. Human Factors

CRM and human model research

  • 4. New technology in ATC

CNS/ATM applications research

  • 5. Crashworthiness

Full scale model test and numerical simulation

  • 6. Conclusion
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SLIDE 3

Flight safety in Japan: Organization structure

MLIT: Ministry of Land, Infrastructure and Transport CAB: Civil Aviation Bureau ENRI: Electronic Navigation Research Institute ATEC: Association of Air Transport and Research

MEXT JAXA Universities Prime Minister MLIT CAB ENRI Airline Operators ATEC METI DA TRDI NEDO Manufacturing Companies SJAC

MEXT: Ministry of Education, Culture, Sports, Science and Technology METI: Ministry of Economy, Trade and Industries NEDO: New Energy and Industrial Technology Development Organization SJAC: Society of Japanese Aerospace Companies DA: Defense Agency TRDI: Technical Research and Development Institute

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SLIDE 4

Safety record in Japan (scheduled flight)

No fatal accident in Japanese scheduled flight for 20 years 1 fatal accident/ 11 million flights = 0.09 per million flights (1985-2003) Number of flight increases nearly twice in 20 years Accidents due to turbulence: 21/42 = 50 %

1984 1986 1988 1990 1992 1994 1996 1998 2000 2002 2004 1 2 3 4 5 6 7 8 x105 Number of flight per year (Domestic and international) turbulence pilot error miscellaneous Cause of accident Number of flight

Fatal accident August 1985

Number of accident from ARAIC report ARAIC: Aircraft and Railway Accidents Investigation Commission

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SLIDE 5

Cabin Safety

Airline operators made efforts to prevent cabin injuries due to turbulence. Seatbelt fastened while seated Flight attendant procedures Handhold installation Sharing turbulence information with other aircraft It is difficult to prevent all the cases, especially those due to Clear Air

  • Turbulence. (CAT)

JAXA researchers challenge CAT warning system.

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SLIDE 6

Production model

Turbulence detection by Lidar: Plan

JAXA’s Challenge: Development of an airborne turbulence warning system for jet transports which can detect clear air turbulence (CAT) up to 5NM (9.2km) at cruise altitude (30,000–40,000ft).

Clear Air Turbulence L a s e r B e a m

2004 2006 2008

Development of turbulence detection / warning algorithm 3NM experimental model 5NM Experimental model 1NM Experimental model Prototype of turbulence warning system for jet transports High power / High efficiency Improvement for jet transports New modulation method for long distance measurement Turbulence (CAT)model Turbulence detection / warning technology wind remote sensing technology (Doppler Lidar)

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SLIDE 7

All the optical components are fiber-based and they are connected by optical fiber. 1.5 µm all-fiber pulsed Coherent Doppler Lidar (CDL) system

20° Laser window

Beechcraft 65 research aircraft with the 1NM experimental model

Wavelength 1.54µm Laser power (Peak) 10W Pulse repetition frequency 50kHz Pulse width 1µs Range resolution 150m Beam diameter (1/e

2)

50mm

Key points of onboard CAT warning system Eye safety Compact and low power Reliable

1NM experimental model

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SLIDE 8

1NM experimental model

Steering mirror Transceiver

  • ptics

Laser transceiver Signal processor Scanner Scanner controller Optical fiber

2002

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SLIDE 9

Level flight, V=120kt, h=5,000ft.

Laser beam

40 45 50 55 60 65 70 75 80 0.5 1 1.5 2 2.5 Range (km) Air Speed (m/s) 2 4 6 8 10 12 14 16 Detectability (dB) Air Speed Detectivity

5 10 15 20 25 30 1000 10000 100000 1000000 Aerosol density (/little) Detectability (dB)

Measured airspeed and detectability (Level flight, h=5,000ft) Correlation between aerosol density and lidar system detectability (150m range bin)

Flight test evaluation

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SLIDE 10

鉛直シア

constant pitch angle of 10° Lasar beam

150 300 450 600

Pitot tube

  • 10
  • 8
  • 6
  • 4
  • 2

2 4 6 8 10 750 1000 1250 1500 1750 2000 2250 2500 pressure altitude (ft) wind speed (m/s) Lidar (0.15km) Lidar (0.3km) Lidar (0.45km) Lidar (0.6km) TAS

Wind measurement results (preview data compensated with pitch angle)

Flight test evaluation

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SLIDE 11

Further development: 3-5NM experimental model

  • 3 NM model (100W) is under development, flight evaluation of

which will be in 2006.

  • JAXA’s researchers study CAT warning system from Lidar data

– Detection method and warning algorithm – Collaboration with computational fluid dynamics researchers and meteorologist

  • Turbulence prediction will be in their future scope
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SLIDE 12

Lidar Application to Helicopters

Type 1 Type 2 TAS Sensor Turbulence Sensor

measure 2 or 3 axis airspeeds even in hover 2 or 3 axis wind speeds measurements 1−2km detection range Multiple observation points Real-time pilot display 2 or 3 axis airspeeds measurements >100m detection range detect severe local turbulence

Helicopter is a good application of Lidar low velocity low altitudes detection range is short aerosol density is high

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SLIDE 13

Helicopter application of 1NM experimental model

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SLIDE 14

Real-time Cockpit Display

Wind Display Wind speed & direction LOS components

  • f wind speed

TAS Indicator Horizontal 2-axis airspeed with limitations

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SLIDE 15

Human factors

A railroad accident, which killed 107 people raised public interest on human factors. The train passed a curve at a speed of over 115km/h, the limitation of which is 70 km/h. At the same period, a series of incidents

  • ccurred in Japanese major airline companies

more than previous years. CAB organized a committee to assess the safety status. It recommended to reconsider the followings. Risk Management System Safety information Crew Training Procedures and manuals Audit by government

from Asahi News Paper

Railroad accident, April 25 2005

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SLIDE 16

Human factors research: CRM skill measurement

  • JAXA researchers propose CRM skill

measurement method to make CRM training more effective.

CRM skills rating sheet

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SLIDE 17

Human factors research: Human model application

  • Human model introduces quantitative evaluation for pilot workload.
  • JAXA researchers collaborate with Sun Jose State Univ. on this subject.
  • They plan to apply their tools to Japanese domestic small passenger

transport development

  • Flight data review with a human model as a reference will be a next step
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SLIDE 18

New technology in ATC

CNS/ATM applications research JAXA constructed a new technology experimental model to evaluate the concept by simulator and flight tests They plan to apply their technology in the two areas Inter-Island flight operation Disaster relief air operation They study reliable GPS navigation system

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SLIDE 19

New technology in air traffic control: NOCTARN

  • JAXA constructed an experimental model of CNS/ATM concept for

small aircraft operation to evaluate it by simulation and flight test. NOCTARN: New Operational Concept using Three-dimensional Adaptable Route Navigation

Data Link Device Air Data Sensor Data Link Device RADAR Wind Sensor Navigation System

position

Surface Wind

VFR Traffic

Airborne System Ground System

MFD ATC W/S

Airspeed, Altitude

CPDLC msg ADS-B msg CPDLC msg. ADS-B msg

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SLIDE 20

HLA network

Scenario Federate

Scenario Wind sensor

Aircraft Federate Wind Federate

Wind

Aircraft Federate

MuPAL-ε MuPAL-α

Pseudo aircraft

datalink ATC workstation

N-Station Federate

DL

N-Station Federate N-Station Federate N-Station Federate

Flight Tests

NOCTARN: Experimental model setup

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SLIDE 21

NOCTARN: MFD

Operations Concept

Guidance Com. Navigation CDTI CDTI

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SLIDE 22
  • Ground evaluation test with

ENRI’s air traffic control simulator

  • Flight test

– at Taiki airfield (for experiment) – Helicopter and Airplane – Cases: Non-towered operation/Towered operation Flight Tests

NOCTARN simulation test and flight test

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SLIDE 23

Application plan: DREAMS

  • JAXA plans to collaborate with FAA

introducing Capstone technology

  • DREAMS: Distributed and

Revolutionary Efficient Air Safe Management System

  • Inter-island flight operation is a

candidate of the future application

FAA Capstone

Airports in Okinawa Islands

(route map from JAL home page ) (from Capstone home page )

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SLIDE 24

Disaster relief

  • Disaster relief operation is another candidate of the application
  • Japan has experienced strong earthquakes, in which disaster relief

by air, especially by helicopters, is essential.

  • Data communication network and high density operation are most

required in the operation

基幹防災拠点 (空港、基地等) 中核防災拠点

防災拠点

公園、グランド等

防災拠点 防災拠点 防災拠点 防災拠点 防災拠点

給油・整備 給油・整備 物資輸送 人員輸送 物資輸送 人員輸送 救急搬送

過密運航

過密運航 過密運航

879 Total 9 Doctor Heli. 46 Coast Guard 95 Police 69 Firefighting 660 Defense Force Number Organization

Number of aircraft in possible relief operation

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SLIDE 25

Navigation system research

  • GPS navigation research since eighties
  • Fully automatic take-off and landing flight

experiment of a spaceplane model vehicle HSFD installing GAIA in 2002 GAIA: GPS Aided Inertial Navigation Avionics

  • Integrity assurance:

HSFD-GAIA(GBAS), MSAS-GAIA(SBAS), µ-GAIA (INS integration)

  • study on miniaturization

µ-GAIA (2004) MSAS-GAIA (2004) HSFD-GAIA (2001) HSFD (2002)

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SLIDE 26

Cabin Safety: Crashworthiness research

  • JAXA researchers challenge crash numerical simulation technique

establishment for aircraft crashworthiness

  • Their goal is cabin safety improvement to increase survivability in case of

accidents Components Substructure Full-structure

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SLIDE 27

International collaboration: ATR42-300 Drop Test

Conducted by FAA William

  • J. Hughes Technical Center
  • n July 30th, 2003.

JAXA provided Experimental Seats With Shock Absorbing Devices.

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SLIDE 28

MH2000 Crash Test, February 25, 2004

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SLIDE 29

MH2000 Crash Test, February 25, 2004

JAXA collaborates with MHI in numerical simulation of the test test Numerical simulation They plan to apply their numerical simulation tools to future development, such as a small passenger transport and helicopter.

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Conclusion

Japan maintains good record in aviation safety. A Series of incidents occurred early this year, however, raised concerns about major airlines’ safety status. They reminded us the influence of deregulation and competition between airlines. Further activities for safety promotion including basic research are necessary. JAXA researchers study, Turbulence detection and warning system development Human factors research CNS/ATM new technology application Numerical simulation for crashworthiness They will present their results in 2006 ICAS, Humburg Germany.

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SLIDE 31