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 boardlevel 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: mitc@moog.com
Phone: +91 80 3372 8000
Fax: +91 80 4120 8840
Web: www.moog.com
Electrical Engineering CAPABILITIES: ILC3000 Asset Tracker Actuator SOV Driver Board 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. Analog Interface Module ACHIEVEMENTS: PWB Layout High Voltage Testing 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 Software 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. ERP Test Case Results MDTE AutoReview Simulink OFP MCMS Commercial Actuation 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 Product Developments Flat & Slat Control Lever Product Lines 
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Variable Air Handle 
High Lift Actuation Systems and Components Primaries Flight Control Systems and Components Cockpit Control Units Core Capabilities 
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B787 High Lift Gear boxes Requirement Management Product Development Project Management Requirement Management Design Analysis Design Core Enablers 
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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 Lean & CI Engineering Standards Growth Roadmap Smallest Position sensor Integrated Servo actuator‐ 002 Integrated Servo actuator‐ 004 CAPABILITIES: 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 Low cost Linear sensor Low cost Angular sensor 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
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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. Test Software 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. 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) 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 Embraer‐Endurance Test Software TEST SOFTWARE PLATFORM: Component Test Software (CTS) Platform Common Test Console (CTC) Platform Portable test Console (PTC) Platform A350 High Lift ATP/QTP Test Command Based ATP Engine Platform 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.