MOOG MOOG India Technology Center
We are pleased to introduce you to the Moog India Technology Center (MITC), located in Electronics City, Bangalore. MITC was inaugurated in
2007 with the intent to become a Design Center for Moog’s Aircraft Group.
Since that time, MITC has achieved AS9100 Rev C certification, CEMILAC
certification and established a state of the art Aerospace Qualification Lab.
MITC’s staff has grown to just under 300 employees, most of them
Mechanical, Electrical, Software, or Test Engineers, all focused on the
design, development, and integration of precision motion control systems.
Currently, MITC is actively involved in the design, development, and
qualification testing of the Flight Control Actuation Systems for the Boeing
787, Airbus A350, Comac C919 and Embraer programs.
MITC has been recognized for significant accomplishments in several
domains. MITC’s Software Engineering group has been recognized by
Boeing and the FAA for the integrity of its DO-178B processes, and the
accomplishment of supporting five aircraft Level ‘A’ certifications in one year.
The System Test Engineering group develops state of the art test systems
to support development and qualification testing of motion control systems
and components. MITC’s Electronic Hardware group is involved in board-
level design and development, as well as a robust obsolescence
management service to Moog’s global businesses. The Mechanical
Engineering group has developed strong design and analysis capabilities
that cover hydraulic and electromechanical systems and components, as
well as supporting Moog’s Global Supply Chain organization.
You can contact us at:
Moog India Technology Center, Plot No.1, 2 & 3, Electronics City Phase 1, Hosur Road, Bangalore – 560 100, INDIA. Email: [email protected] Phone: +91 80 3372 8000 Fax: +91 80 4120 8840 Web: www.moog.com
ILC3000 Asset Tracker
Actuator SOV Driver Board
Analog Interface Module
CAPABILITIES: The main capabilities of Electrical section are in design and development of Digital,
Analog, Power, Component Engineering, PWB and Packaging.
Expertise in Requirement and Design based V&V for digital design as per DO‐254
standard. Successfully completed multiple SOI Audits for Boeing and Airbus programs.
Design and development of Processor and FPGA based cards.
Perform VHDL synthesizable coding and V&V.
Schematics design and design analysis for various flight cards for C919, Embraer used in
different LRU’s.
Expertise in electronic part symbol/footprint creation.
Expertise in electronic part Obsolescence Management, Global Part Management,
REACH analysis for different MOOG sites.
Expert Layout Team capable to perform complex board designs including high density
processor boards, analog boards, high voltage and high power design.
Thermal, Vibration and Shock analysis of different Electronics packages.
Creating and Revising of Component Maintenance Manual (CMM / ACMM)
Design and Development of MOOG Test Engineering Hardware.
Process adherence to comply with DO254 Standard, FAA and EASA guidelines.
PWB Layout
High Voltage Testing
ACHIEVEMENTS: 787 EMCU DCE FPGA ‐ SOI#3 V&V Audit during July‐2015 at MITC.
ACM card schematic design and PWB Layout design for multiple programs.
C919 – Schematic and PWB design of ACM, FB and MB
C919 – ACM De‐rating analysis, power rating analysis and FB Transient Analysis.
Embraer ACM board Layout.
ILC3000 Asset Tracker design and development
Design and Development of ARINC‐429 simulator card (48 TX and 24 RX channels).
Embraer – Timing Analysis of CCM4, CCM5 and CCM6 processor cards.
A350 Saber analysis.
HV / HA lab testing of A350 boards.
A350 EM – Burst pressure Analysis.
MOCA‐ Mitigation of Obsolescence Cost Analysis.
New VLS Tool Development.
PWB Layout: 6CH DDV Drive AIM Card, ARINC simulator Board,
Technical Publication: CCA CMMs for 747 LCE, CCA CMMs for 787 EMCU, Slip Ring
CMM for MCG, Skew Linkages CMMs for 787‐8, 787‐9, CMM Support to A350 program.
Digital VnV Process Flowchart
REACH Analysis
Electrical Engineering
MITC Software team has the unique distinction of certifying five safety critical software projects in a single year. The
certifications were given for the flight control laws for the various aircrafts as per DO178B Level A. MITC Software team
has worked on the Model Based Testing of Boeing 747‐8 Freighter and the Intercontinental versions, Gulfstream, G280,
G650, and G500 flight control laws. Currently MITC is working on the COMAC and Embraer aircraft programs.
The control laws provided by Boeing were converted to Simulink® models for the Verification and Validation activity at
MITC. MITC certified the Airbus A350 actuation system with control electronics. The SCADE® designed controllers are
converted to Simulink models for the Verification and Validation of the electrohydraulic (EH) and advanced electro‐
hydrostatic (EHA) actuators, electronics, and software.
Model Based Test follows a series of processes based on a set of proprietary tools developed at MITC. These in‐house
tools are today qualified for use on safety critical projects. The Simulink model is used by the Expected Results
Population (ERP) tool to generate Test Cases. The Test Cases are automatically reviewed by the Auto Review tool which
checks for block requirements coverage. The Moog Desktop Test Environment (MDTE) reads test cases and injects it
into the OFP build on the Moog On Board computer. All data and results are configured in the Moog Configuration
Management System (MCMS) developed in‐house at MITC.
MITC has developed the platform software that is a certified operating system for the three channel redundant
computer. A newer version of the software caters to the new high speed processor based computers developed by
Moog for the Embraer program.
MITC has developed a helicopter control law as an R&D initiative. MITC has developed an OBC in loop system test
platform to validate this three channel redundant control system. Moog is today venturing into the robotics market by
supplying high reliability smart and compact actuators for robotic application. The Integrator Servo Actuator
communicates using EtherCAT and CAN Open protocols.
Engineering Applications
The Software Engineering has an IT component with expertise in developing Web and Windows based Applications
using .Net and Java platforms. This team provides Process Automation Solutions to all Moog sites thereby improving
their efficiency. The software is developed following AGILE and SCRUM methodology for Project Management. The
team has core skills on Java, Groovy Grails, MVC, .NET, SQL Server, JavaScript, Jasper reports, Google Graphs,
Hibernate and Spring Security, Twitter Bootstrap, JSON ,LINQ, WCF, AJAX, SharePoint, JSon and JQuery.
MCMS
OFP AutoReview Simulink
Results MDTE Test Case ERP
Software Engineering
Product Developments
MITC is responsible for performing front‐end design and
development activities for High lift Actuation systems,
Primary Flight Control systems and Cockpit control
units. The group has significant experience in Product
development, Project management and Design &
analysis activities. The group has been playing key roles
in executing Commercial Aircraft programs since its
inception. In addition to executing the NPI activities for
current programs, the group is also engaged in
developing many products which are key to the success
of cost down initiatives of the Organisation. The group
has modeled the application of Lean and Continuous
improvement (CI) approaches in day‐to‐day Engineering
activities.
Project Management
Flat & Slat Control Lever
Variable Air Handle
Product Lines
High Lift Actuation Systems and Components
Primaries Flight Control Systems and
Components
Cockpit Control Units
B787 High Lift Gear boxes
Requirement Management
Analysis
Core Capabilities
Product Development
Project Management
Requirement Management
Design
Analysis
Core Enablers
Lean and Continuous Improvements
Robust processes (Turnback and Escape
addressal system, standardisation of basic
engineering practices etc.) ensuring
sustainable maturity and growth
Holistic goals and objectives
Plan to Growth and Growth to Plan
Design
Lean & CI Engineering Standards
Growth Roadmap
Commercial Actuation
Smallest Position sensor
CAPABILITIES:
Integrated Servo actuator‐ 002
Integrated Servo actuator‐ 004
Low cost Linear sensor
Low cost Angular sensor
Idea to physical Prototype in short period
Ideation and Interpretation of Idea
Concept Design
Detail Design
Manufacturing (in‐house & outsourced)
Assembly & Proof of Concept Tests
New product development
Design and development of Electrical, mechanical and
hydraulic components for Aerospace, Robotics and other
Industrial applications.
High voltage testing
Partial Discharge testing for risk mitigation
ACCOMPLISHMENTS IN PRODUCT DEVELOPMENT:
Hydraulics and components
Integrated Servo Actuator (ISA) with Position & Force
control
Series Elastic Actuator (SEA)
Hydraulic Integrated Rotary Actuator (HIRA) (in concept
stage)
Design for Additive manufacturing
Thumb Remote Electronics Unit (REU) with digital closed
loop control & Local Area Network of sensors
Electric motors and sensors
LVDTs, Single & Dual channel
RVDT and Resolver
LFM – Micro Direct Drive Valve (DDV)
Low cost & high performance electric motors
Hall effect sensors (Linear & Rotary)
COTS+ Motor
SEA Motor assembly
Hydraulic Rotary actuator
Robotic Arm
Thumb LFM
Segmented armature motor Low cost rotary sensor RVDT
Qualification / Performance Test Engineering
CAPABILITIES: Qualification testing of Hydraulic, Mechanical actuators & Gear
Transmissions for Commercial Aircrafts.
Product engineering support to Primary actuation system & High lift system
for Commercial Aircraft applications.
Component level Qualification testing for Commercial Aircrafts (Hydraulic &
Mechanical).
Build and set up‐test facilities like pump rigs, Hydraulic Control Panels, Test
rigs, auxiliary facilities & TPM activities.
Test data analysis and Test report generation.
Acceptance, Qualification test plans, procedure write ups and review.
Disassembly and Assembly of Hydraulic, Mechanical actuators & Gear
Transmissions for component level inspection.
Assembly and Production Test Support for Moog Production Hubs.
Perform environmental qualification testing of Hydraulic & Mechanical
actuators using external facilities.
Support Qualification testing of Hydraulic, Mechanical actuators & Gear
Transmissions at different AG sites.
Process adherence to comply with DO160G Standard, FAA and EASA
guidelines
Qualification Lab is AS9100 certified.
ACHIEVEMENTS: Successfully completed:
A350 PFCA – DDP and Test Reports for OB Aileron SC, Elevator SC, Rudder
SC, IB Aileron SC, Spoiler SC, Elevator EHA, Rudder EHA, IB Aileron EHA and
Spoiler EBHA
A350 HL ‐ Endurance Test and Test Reports for BGB25, KGB40/63, SGB,
BGB19, WTB, TBGB.
A350 HL ‐ Fatigue Test and Test Reports for BGB25, KGB40/63, SGB,
BGB19, LBA2, LBA4.
A350 HL ‐ Disassembly and Inspection for BGB25, KGB40/63, SGB,
BGB19, LBA (STA1, STA2 & STA3).
787‐9 ‐ Full Endurance test for IB Spoiler and Elevator.
G280 ‐ Endurance Test and Test Reports for Multi‐Function Spoiler
Actuator.
TEST FACILITIES: Pump Systems Ambient fluid temperature of 120 gpm flow at 5000 psi (Hyjet Oil). High fluid temperature (Ambient to +120°C) of 40*2 gpm flow at 5000 psi
(Hyjet Oil). Ambient fluid temperature of 90 gpm at 3000 psi (Red Oil) Portable ambient high pressure pump system (8000 psi). Total 12000 sqft of lab space (Qual lab 1, 2 & 3) Semi‐automated dual source hydraulic control panels/hydraulic test manifolds. Oil at low temperature test facility (up to ‐55°C) Thermal chambers to meet DO160 standards for environmental tests. Fully equipped Disassembly & Assembly lab Contamination analysis lab adhering to AS4059 standard Safety Measures ‐ Eyewash stations, Safety showers, Safety glasses, Gloves, Shoes and Aprons.
Test Solution Engineering
Capabilities: Requirements Management: Understanding Customer requirements and allocating these
requirements to various subsystem(s) / component(s). Derive Test System requirements to meet
higher level requirements. Ensure the requirement compliance through verification and validation.
Maintain multi‐tier traceability using IBM Rational DOORs tool.
Design & Development: Design, Development and Deployment of Performance, Acceptance and
Qualification Test Systems for Primary, Spoiler, High Lift and Electronic Control Units, which includes,
Test Stand: 3‐D modeling and detailed design of mechanical rig, assembly tools to support UUT
mounting and assembly during various qualification tests.
Tools: UniGraphics, AutoCAD, TeamCenter, Ansys, Solid Works
Test Console‐Electronics: Electronic controller, Motor Controller Unit and Interface Cables to UUT
and test stand sensors/signals.
Tools: Cadence, AutoCAD, MS Visio
Platforms / R&D: iCON ‐ MC600 based low cost controllers, xPC Target based low cost simulator.
Modeling, Simulation and Analysis: Development of Impedance Rig (Dynamic Damping & Dynamic
Stiffness Rig) model. Perform Simulation & Analysis for selecting the load system components and
finding appropriate rig stiffness to meet the test requirements.
Tools: Matlab/Simulink, xPC Target, dSPACE Control Desk, MAST (Moog Analysis and Simulation
Toolbox)
Process Integrity: Develop, Train, Assess and Improve System Development Life cycle processes. Test
Equipment Design Standard (TEDS) provides standard design guidelines for test equipment
development.
Tools: JIRA (Problem Reporting), SVN (SubVersion), E/EO release tools, Moog Custom reporting
tools (WO# tracking)
Production Support: Support production problems, upgrade legacy test systems and components to
ensure test system availability.
Accomplishments:
Test Rigs: Design and Development of mechanical and hydraulic test rigs for,
Endurance Test Vibration/Environmental Test Acceptance and Functional Test Fatigue Test Test Electronics: Design and Development of automated test equipment (ATE) for,
SC/EHA/EBHA actuators High Lift systems Hydraulics pumps and motors Electronics boxes / boards Modeling & Simulation:
Develop Test System Simulator (TSS) to support HIL simulation for Primaries actuation system. Develop High Lift system (Flap and Slat) approximate models to support System Software
Workstation integration. Load system control analysis using Delta P method. Process Integrity:
Develop processes for System Development group Provide training on processes and reasons for adherence. Conduct periodic process audits to ensure process adherence. Key link between System Development and Quality Assurance group.
C919 SSW HLS Modeling and Automation Test Software
ACCOMPLISHMENTS: Embraer Automated ATP test Software C919 HL GRA ATP test Software C919 HLS SSW Modeling and Automation Test Software. A350‐900 HL Qualification Test Software (NI RT/MC600) A350‐900 HL LBA Qualification Test Software A350‐900 HL Automated ATP Test Software A350‐1000 PFCA Automated ATP Test Software A350‐900 PFCA Automated ATP Test Software 787‐10 Automated ATP Test Software G280 Automated ATP Software A350 Hipot Test Software A350 EM Automated ATP Test Software (ATP, CAL, Selftest, HASS)
CAPABILITIES: Design and Development of Automated Test Software for,
Flight Control Actuators (SC/EHA/EBHA/HCM/SCM)
High Lift Systems
Hydraulics Pumps and Motors
Electronic Boxes/Boards (FCRM,EM, FSECU, FCC)
Hipot Systems
Servo Valves and Rudder Pedal
Design and Development of Test Software Tools
Expertise: NI LabVIEW, NI TestStand, NI VeriStand, Codesys,
DSpace, Python, Ruby, Lua, Origin etc.
Embraer‐Endurance Test Software
TEST SOFTWARE PLATFORM: Component Test Software (CTS) Platform
Common Test Console (CTC) Platform
787 SEMA ATP Test Software G7 Rudder Pedal ATP and QTP Test Software Servo Valve Automated ATP Software A350 PCU Data Handler Tool Dual Source HCP Software (MC600) SVN Based Production Software Configuration Management Tool Generic QDAS DFQ Generator for CTS Platform. Checksum Buster Plugin for Legacy Softwares
Portable test Console (PTC) Platform
Command Based ATP Engine Platform A350 High Lift ATP/QTP Test
Software
SVN Production SW Config Tool Generic QDAS DFQ Generator
Quality Assurance
Highly Qualified and Competent Professionals Assuring Quality in all the Processes that Exceed Customer
Expectations.
KEY COMPETENCIES:
MITC Quality Engineers Certified by Boeing and Embraer for Conformity Inspections.
MITC dedicated DMIR (FAA delegation) support from Baguio for Test Setup Conformity.
Certified Trainer for Article and Test Setup Conformity.
Train and qualify the competent technicians and engineers and issue self‐verification stamps.
Source Inspection support to Asia Supply Chain.
DO‐178 and DO‐254 Process Assurance.
Test Software