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Logic S.p.A. Company Presentation

November 2016

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LOGIC Sistemi Avionici

Number of Employees: 108Total Sales 2015: 21.3 M€

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Our History by main events

• Logic is an Italian company based in Cassina de’ Pecchi, in theoutskirts of Milano.

• It was founded in Milano in 1962 and it grew as a Company capableof developing and producing state-of-the-art electronic systemsdedicated to embedded avionic applications.

• In more than 50 years of activity our know-how has increasedgaining multiple experiences for different kinds of electronicapplications for on-board products on fixed and rotary wingsplatforms.

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Today Major Customers

- Airbus Helicopters - Boeing Helicopters- Firstec- Leonardo (former AleniaAermacchi)- Leonardo (former AgustaWestland)- Leonardo (former Selex ES)- Kawasaki HI - Thales Communications and Security - US Army and US Navy

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Quality System

LOGIC’s Quality System is certified by:- ENAC (POE - PART 21)- ENAC (MOE - PART 145)- FAA (FAR 145)- TCCA (CAR 573)- UNAVIA / TUV (UNI EN ISO 9001: 2008)- UNAVIA / TUV (UNI EN 9100: 2009)

LOGIC’s Quality System is qualified by:- LEONARDO Helicopter (AECMA EASE)- ARMAEREO (AQAP-2110/AQAP-2210)- BELL Helicopter (Bell Quality System) - BOEING (BQMS) - HINDUSTAN (Hindustan Quality System)

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LOGIC’s Capabilities

System design support to the Customer.Full Product Design according to the state-of-the-art military and civilstandards including:

• Hardware, Software, RMST, Electrical, Mechanical Design• Prototyping• Qualification according to the most stringent requirements• Test Equipment design and manufacturing• Product Manufacturing• Support of the Product

In order to do so, Logic can count on its own state-of-the-art internalDesign and Development Tools and Qualification Facilities.

We gained significant experience on DO254 and DO178 up to level Afor safety involved design.

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Temp./Altitude Test

Test Equipment

RF FILTER TESTER AGE for Testing Filter characteristic

of EFA loads release unit

PU STTEAutomatic Test System forPYLON UNIT - SMS M346

AGP + TPS NH90Automatic Test System for

FMS NH90

I/O MODULE TEST SETSemi-automatic test system for

IO Board of SMC M346

Manual or Automatic test equipment developed to support project developmentand/or unit test both for LOGIC or third parties products.

Activities supported with the preparation of the relevantmanuals and technical documentation.

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Development & Qualification Facilities

Mechanical Test

EMI/EMC Laboratory

Lightning Test

Optical Characteristics

Temp./Altitude Test

Temp./Humidity Test

Salt Fog Test

Temp./Altitude Test

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4 Product Lines4 Product Lines

Cockpit & Processing

Fuel Management

Products Overview

Power Management & Control

Electromechanical Actuation

Logic can leverage its long time experience in electronic for avionics applications todesign a wide variety of products. Its own legacy, combined with the new ongoingdevelopments, makes the Logic’s product catalogue important including hundreds ofequipment.

The products are currently on-board of well-known platforms both for fixed and rotarywings, some with a long service history and still maintained by Logic.

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From single function dedicated units to multi functions data acquisition managementand concentrator units based on high performance electronics.Cockpit units from discrete information up to ruggedized AMLCD for user-friendlyMan Machine Interface.

• Leonardo Aircraft M346• Leonardo Helicopter A109 – A129 – A139• Airbus Helicopters SUPERPUMA MKII+

• Leonardo Helicopter EH101• Hindustan ALH• Thales Comms Various

Cockpit & Processing

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Smart Control solution

Based on Small size Active Matrix Display differentsolutions are implemented for specific control function.• Proprietary Rugged AMLCD process, for hard environment

performances

• Full Graphic design capability

• Complex integrated function

• Multi-page operation

• Flexible interfacesGHD

RCU

Cockpit & Processing

WCP CCU

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Vibration Management System Computer (VMSC) for Active Control of Structural Response

• 16 Analog in channels, configurable to be interfaced toaccelerometers or strain gauges sensors

• 8 Analog in channels configured for strain gauge sensors

• 4 Actuator out channel for electro-valves

• Analog conditional channels with SW programmable gainsand 16bit A/D conversion

• Dual channel architecture, Actuator and Monitor:

• Monitor based on DSP SHARC, 450MHz, 2.7GFlops, 5MbitRAM expandable

• Actuator based on DSP C6000, 456MHz, 2.7GFlops, 32MBRAM, 4GB EMMC memory

• Analog front-end managed by an ARM Cortex M4processor

Cockpit & Processing

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Full spectrum of low and medium power solutions ensuring smart PowerManagement.

Enhanced Solid State Power Distribution based on Solid State Switches with highperformance management capabilities.

• Leonardo Aircraft M346• Leonardo Helicopter EH101• Airbus Helicopters NH90 – EC225

Power Management & Control

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A segment on which Logic has spent significanteffort for acquisition of dedicated competence isthe Solid State Power Distribution with all theadvantages of this smart solution.

Solid-State Power Controllers (SSPC)

- Low (1A-5A) and High (5A-25A) current channels

- Outputs paralleling for higher current

- Selectable pre-defined trip curves by channels

- Overloads and short circuits protection

- Programmable current rating for each channels

- PWM and soft start operations for each channels

- Can Bus Arinc 825/826 interface

Power Management & Control

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Electromechanical Actuation

Actuator/Control LeverFrom mechanical Control Levers for different applications upto Electro Mechanical Actuation.Intelligent and smart Electro Mechanical solutions based onstate-of-the-art electronics.

• AAEM/ALN/EMB AM-X• Leonardo Aircraft M346• Leonardo Helicopter EH101

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Engine Control SystemIt combines, within a single application, electronic design capability (analogue loop)and lever design.

• The Boeing Co. CH47• The Boeing Co. H46

Electromechanical Actuation

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Following the interest of the market that, for different reasons, is moving with always largerinterest to all electrical actuation, Logic has matured the know-how necessary to includealso the electrical actuation capability in its basket.

Main features of electrical controlled actuation are:

• Possibility to easily design smart actuator, following the concept of “distributedintelligence”

• Possibility to implement complex control law of the actuators

• Possibility to easily change the behavior of the actuator through new SW

• Easy maintenance operations (calibration, replacement, etc.)

• Full BITE function � HUMS

• Performance independent from the ambient temperature

Electromechanical Actuation

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Actuator Control Unit (ACU)

In the course of a research program (Industria2015), LOGIC have developed an electronicequipment (ACU) that drives a brushless motor tocontrol the extension/retraction of the helicopterlanding gear legs

− The ACU will drive a brushless motor with amaximum power consumption of 800W

− Dual channel technology, one based on highperformance microcontroller (actuation) andone based on programmable logic device(supervisor)

− The ACU manages an electromechanical braketo stop any legs movement

− FREE-FALL management

− HUMS data management

Electromechanical Actuation

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ACA Rotary Actuator

• Operates under an opposite torque of 260Nm

• Electrical operating stroke: 193.7°

• Two position switches, one for each end of theelectrical stroke

• Manual interface to assure, by a manual crank rotation,the output shaft full stroke movement in case of powersupply unavailability

• 60000 cycles without replacement or repair of majorstructural components

• Power Supply 18Vdc - 30Vdc

• Power Consumption 18 Amp. Max

Electromechanical Actuation

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Wide range solutions based on passive or active probes withappropriate signal conditioning, including multiple variableprocessing for Fuel Gauging and Fuel Management up tocomplete Fuel Systems Solutions.

● Leonardo Aircraft M346

● Leonardo Helicopter A109

● Airbus Helicopters H135 - H145 - PUMA - NH90

● Hindustan SARAS

● Firstec MUAV – MAR UAV

● Kawasaki HI BK117

Fuel Management

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NH90 Fuel Management System

Fuel system is composed of:

− Main Computer− Backup Unit with pilot/co-pilot interface (NVIS Class A Type I)− External fuel ground control panel dedicated to refuel

operation− 6 active probes (microprocessor equipped), 2 with optical LL

The system manages 25 devices (electromechanical valves,pumps, sensors for refuel, transfer and fuel dump)

• SW DO178B level B• ARINC 429 interface to the Avionics

The system compensates for the flight attitude with the datareceived from Avionic. Provision to perform the compensationdirectly with built-in flight attitude sensor, based on MicroElectro-Mechanical System (MEMS), is already available.

Fuel Probes Fuel Shut-Off Valve & Pump

Management Computer, Ground & Cockpit Panels

Fuel Management

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Fuel Probe with High Level Sensor and Low Level Sensor

Active Fuel Probes

- Telescopic probes

- Capacitive technology (no moving part present)

- Ultra Low Power Microcontroller

- 2 wire interface (Data over Power Line)

- High level sensor with different technology

- Low power consumption (20mA)

- Crash landing controlled collapse structure

- HIRF, NEMP and Lightning harsh environment proof

- Qualified in accordance with NH90 requirement specification

- Built-in water detection functionality

- Independent Low Level Warning (Optional)

Fuel Management

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Fuel Probe

XFU equipment

Fuel Gauging and Management System for MAR-UAV

- 9 Passive capacitive probes (no moving parts)- 1 Computing equipment (XFU)- Low Level separated sensor- Compensator for mass computation- RS 422 interface to the Avionic- Lightning protection- SW developed per RTCA/DO178B level C- Flight attitude compensation- Derived from M346 Fuel System Gauging

UAV Fuel System Architecture

Fuel Management

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NH Industries - NH90

• Advisory Panel (NVG)• Deicing Control Board• Store Management System• Folding Automatic Controller• Fuel Management System• External Fuel Control System• Emergency Floatation Unit &

Water Immersion Sensor

APN

FAC

EFU

EFCS

SMS

DCB

FMSFMS

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Leonardo Aircraft - M346

• Vehicle Computer (MISCO)• Generator Control Unit • Fuel Management System• Crash Survival Memory Unit•Get Home Display• Engine And Fuel Display Panel• Data Recording Unit• Landing Gear Control Lever• Canopy Actuation System• Stores Management System

MISCO

GCU

FMS CMU

DRUALA

ACA LGL

EFPGHD

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Our Future - Our Strategy

• To leverage existing capabilities• To sustain and expand the product

portfolio • To consolidate relationship with

current Customers• To target new platforms • To access new markets