Next Generation Avionics Solutions for Thailand

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Next Generation Avionics

Solutions for Thailand and Others

A Summary of the Thailand C-130 Avionics Upgrade Program

Chad Williams

Rockwell Collins, Inc.

319-295-7795 cmwilli1@rockwellcollins.com

Thailand C-130 Avionics

Upgrade Program (AUP)

• The Royal Thai Air Force (RTAF) and Thai Aviation Industries

(TAI) selected Rockwell Collins as Prime Contractor to upgrade

12 Royal Thai Air Force C-130H/H-30 aircraft in September

2006

Objectives for

Thailand C-130 AUP

• Reduce obsolescence issues of procuring spare parts for existing C-130 components

• Improve CNS/ATM capabilities

• Reduce avionics maintenance costs

• Provide new Flight Management System

• Reduce pilot workload

• Allow flights between countries under ICAO regulations

• Support both day and night operations

Rockwell Collins’

Responsibilities

Engineering Design

And Development

Installation Design

Onsite Field Service &

Logistics Support

Ground &

Flight Testing

System Integration

Technical

Publications

Lab/Bench Test

- S/W Formal Qual. Testing

A-Kit & B-Kit Hardware

Deliveries

Aircraft Installation

- RC Field Service Staff

- TAI Install Technicians

Pilot &

Maintenance

Training

Thailand C-130

Program Schedule

Oct-06 Jan-07 Apr-07 Jul-07 Oct-07 Jan-08 Apr-08 Jul-08 Oct-08 Jan-09 Apr-09 Jul-09 Oct-09 Jan-10 Apr-10 Jul-10 Oct-10 Jan-11

Contract

Award

Oct 2006

Avionics Design & Development

12 Months

Installation Design

8 Months

Prototype

Installation

6 months

Aircraft

Testing

Production Aircraft Modifications

• Major Milestones

– Contract Award – Oct 2006

– First Flight – April 2008

– Prototype Complete – August 2008

• As of Sept 2010, 9 out of 12 aircraft successfully modified and back in operation

• All 12 aircraft scheduled to be completed by April 2011

Aircraft Modification

• Installation Being Performed at Takhli Air Force Base in Thailand

Aircraft Modification

• Onsite Wire Harness Fabrication

Capability

• Onsite Sheet Metal Modification and Fabrication Capability

Thailand C-130 Cockpit

(Before Modification)

Thailand C-130 Cockpit

(After Modification)

Thailand C-130

Installation Team

Rockwell Collins

Flight2 TM Avionics System

Thailand C-130

Systems Upgraded

• Flight Management System

– CARP/HARP, Search &

Rescue Patterns, Integrated

Control of Systems, RNP-0.3

• Multi-function Displays

– LRU Reduction of 60%

• Autopilot System

– TSO certification

• Navigation Systems

– Air Data Computer

– Inertial Navigation Unit

– VOR/ILS/GPS

– Radio Altimeter

– DME

• Communication Systems

V/UHF

HF

SATCOM

Intercommunication Sys

• Surveillance Systems

Weather Radar

TCAS

TAWS

Mode S

Digital Map

• Emergency Systems

ELT

Standby Instrument

Pilot/Flight Engineer

Training Class

System Integration

Laboratory (SIL)

• SIL Delivered to Thailand in June 2008 to Enhance Pilot and

Maintenance Training

• Assist RTAF/TAI in Avionics Troubleshooting and Repair

Flight2 TM Benefits

• Meets all current and known future CNS/ATM requirements

– Capable of evolving for future unknown requirements

• Scalable

– Designed to meet multiple price points and capabilities

• Configurable

– Easily adaptable to unique customer requirements

• Large Baseline

– Over 150 C-130’s on contract to draw from for software, system, and installation design (>100 in operational service)

– Over 2000 fixed and rotary wing aircraft in operation with variation of the baseline Flight2 TM

• Obsolescence Management

– Obsolete parts are managed and resolved without impacting customer

– Common building blocks across hardware components ensures long term supportability and repair

CNS/ATM Requirements

Communication

VHF Radio 8.33 kHz Spacing

Mode S Level 2 Enhanced Surveillance

Multiple ATC Data Links SATCOM

• VDL Mode 2

Navigation

• FMI: Frequency Modulation Immunity

• RNP: Increased Navigation Accuracy

• RVSM: Reduced Vertical Separation

• RNAV: Flexible Routings

Surveillance

Mode S

ACAS II: Airborne Collision Avoidance

TAWS: Terrain Warning

ADS: Auto Position Broadcast

1997 1998 1999 2000 2001 2002 2003 2004 2005 2006 2007+ 2009+ 2010+ 2012+ 2015+ 2025+

NATS

RVSM

Europe

BRNAV

(RNP-5)

Pacific

RNP-10

Europe

7 States

VHF 8.33

Pacific

RVSM

Europe

ACAS II

WATRS

RVSM

Europe

P-ILS

Europe

RVSM

ATN/VDL2

Europe

Mode S

Elem

Surveillance

U.S.

RVSM

Europe

ELT

Solutions for CNS/ATM Challenges Need to Meet the Required IOC Dates

Pacific

CPDLC

ADS-A

Europe

All VHF

8.33

P-RNAV

SBAS CAT I

TAWS

U.S.

Mode S

TAWS

Europe

Pacific

RNP-4

GBAS

Cat I

Europe

Mode S

Enhanced

Surveillance

Europe

ATN/VDL2

RNP RNAV

U.S.

RNP RNAV

Europe

CPDLC

Europe

GBAS

Cat II&III

VDL4

U.S.

GBAS

Europe

4D RNAV

U.S.

RNP-2

(Requires WAAS)

+ LPV

Approaches

Europe/U.S./Pacific

Civil SATCOM D/L & Voice

2010-2011

ADS-B

Europe/U.S./NAT

Europe

RTA<30 sec

2007-2010 ADS-C

Scalable to Mission

Requirements

 Strategic Airlift

 Unrestricted Global

Airspace Access

 Commercial & Remote

Operations

Mission

Tactical Airlift

Combat Delivery

Humanitarian Aid

Remote Operations

Evacuations

 Special Missions

 Air to Air Refueling

 Search and Rescue

 Surveillance

Requirements

 Worldwide CNS/ATM

 BRNAV

 RNP NAV

 Data Link

 Long Range Comm

 Future CNS/ATM

Functionality

 8.33KHz Spacing

 P-ILS, TCAS II

 ENH Surv ,ADS-B

 Commercial FMS/GPS

 SIDS/STARS

 Digital AP / ADC

 HF and/or SATCOM

 VDL, Displays

 HARP / CARP

 M/TLS or GPS/Tactical

Approaches

 Defensive EW Systems

 MIL FMS / GPS

 HF and/or SATCOM

 Integrated Warning &

Displays

 Radar, TAWS, Dig Map

 Head UP Displays

 MIL Patterns

 Search Patterns

 COMMS / DL

 Integrated Sensors

 MIL FMS / GPS

 HFDL / SATCOM

 Mission Displays

 HUD / Dig Map

Equipment

 ARC-210 or Talon

 HF Radio

 SATCOM

 Datalink

 VOR/ILS/GPS

 ICS

 Inertial Nav Unit

 Air Data

 Radio Altimeter

 DME

 Weather Radar

 TCAS

 EGPWS

 Transponder

 Digital Map

 Autopilot

 Displays

 Engine Instruments

 HUD

 Flight Management

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Customized for Variable

CNS/ATM Requirements

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Rockwell Collins

Integration Experience

Engine Instrument

Display System

• Standard 32 engine instruments

• Hydraulics (Aileron,

Elevator, Rudder, Flaps)

• Multiple

Caution/Warnings

• Condense to single display to depict whatever video input connected (WXR,

Digmap, Camera, etc)

• Can pay for itself in maintenance savings in one year

Benefits of Flight2 TM

Avionics Upgrade

Operational & Safety Benefits

• Compliance with Civil aviation regulatory requirements through 2020

• Increased operational readiness for aircraft & aircrews

• Reduced pilot workload due to integrated displays & controls

• Increased safety margins due to airdrop accuracy

• Increased situational awareness/safety during flight

• Enhanced interoperability with NATO forces

Cost Benefits

• Decreased maintenance and repair costs

• Open Systems Architecture allows for future technology updates

• Increased navigational accuracy decreases missed approaches

• Fuel savings due to availability of preferred routings

• Increased pilot proficiency reduces training costs

• Single Avionics Integrator minimizes life cycle costs

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