In cooperation with 50+ Aviation Engineers & Experts

Partners:

UASystems

UASystems SA, a "think tank" for unmanned and optionally piloted rotary wings (VTOL Vertical Takeoff and Landing) MTOW 300+ kg from the first idea to technology transfer in cooperation with strong partners based at the Swiss Aéropôle, Payerne, Switzerland. Together with our partners, we work with over 50 top experts from the areas of research and development, production, marketing, and certification on our own products and, in the future, for third-party products. As a unit, we also recommend ourselves to our customers and investors.

UASystems SA has more than 25 years of experience with drone technologies. UASystems SA offers an overview of holistic unmanned and optionally piloted rotary-wing aircraft, know-how in the design of a platform, a description of the drive systems, the definition of the autopilot, the GCS ground control station, and the data link. UASystems SA has a large network and relationships with leading global suppliers. There are close relationships with long-term partners and organizations to keep track of the state of the art. UASystems SA has developed its own projects such as the PROVISTA SOS Peyelot system. Work is currently underway on the SKT UAS-OPH, an optionally piloted helicopter with a payload of 300 kg, and on the eZELOS300, an electric VTOL drone for vertical take-off and landing with a revolutionary multi-fuel generator/ range extender.

© Barakat 2019

UASystems

swiss aeropole SA is responsible for civilian

operations at Payerne Airport, and develops a

business and technology park for companies in

aerospace and related industries on a 40-

hectare area located next to the airport’s 2.8

km runway.

The Centre for Aviation (ZAV) in Winterthur, Switzerland, works in an interdisciplinary manner and deals with complex issues in the aviation industry. ZHAW School of Engineering combines various technologies, methods and areas of knowledge with the aim of mastering the challenges of global mobility of the future and researching ways to make it more efficient and safer. Aerodynamics and flight mechanics teams are primarily concerned with the aerodynamic design of aircraft and the resulting optimization of flight and stability properties including augmentation systems. The Center for Aviation has competencies and methods in numerical flow calculations (CFD) and in the implementation of wind tunnel tests. Among other things, a low-speed wind tunnel developed at the Center for Aviation (ZAV) is available for this purpose. ZAV has also expertise in various professional branches of aviation including the development of training tools and methods that are intended to support and relieve people in their work. For example, the ReDSim research simulator is also used for research purposes in the area of human-machine interaction, for example for the use of speech recognition in the cockpit.

Systems integration and structural integrity This department focuses on the integration of complex systems in the field of technology and operations in aviation. Electrical systems play an increasingly important role in the development of new aircraft. These systems must be integrated in order to ensure safe air traffic operations.

KUERZI Aviation AG KUERZI Aviation AG is an EASA-approved design, production and maintenance organization. We design, produce, install, maintain and certify avionic components and complex electrical systems for all aircraft types.

Our engineering team designs certified systems including components from bottom up to aircraft level, including environmental testing (DO-160), software certification (DO-178C) and flight testing with or without our own flight laboratory. We develop EASA STCs and/or EASA Minor Change Approvals and deliver complete installation packages to enable efficient installation. We also validate design data for third countries such as Brasil, Indonesia, Russia and the USA (FAA). EASA DOA PART 21 J Approval EASA POA PART 21 G Approval EASA MOA PART 145 Approval

Portrait The transparencies and aero structure company MECAPLEX, founded in 1948, employs 60 specialists for the aeronautical industry and belongs to the Glas Trösch Group since 2011. The Company has continued to grow due to an innovative spirit, an effective response to customer requirements and commitment on the part of its employees. MECAPLEX transparency solutions are a standard in the aeronautics industry. Leading aircraft and helicopter manufacturers are among its clients. Description Aircraft, helicopter and VTOL glazings MECAPLEX produces mono- or complex multilayer transparencies for all types of aircraft and helicopters. We develop and produce innovative transparency solutions made of acrylic or polycarbonate with scratch-resistant coating. Also in multilayer design. Optional built-in heating system. MECAPLEX is also a key partner for maintenance, repair or replacement of transparencies. Customers and fleet operators in many countries rely on this service. Aerostrucutres Assemblies MECAPLEX is an experienced provider of manufacturing, assembly and inspection technologies for aircraft structural assemblies made of metal or composites. State-of-the-art light construction technologies are omnipresent in the aviation industry and are demanded in numerous segments. The composites comprise low weight with high stability and are increasingly replacing materials such as aluminium. Due to our long years of process competence in the composites segment, Mecaplex customers are provided with all services from the development idea to SOP all the way to the first components for serial production. All of this from a single source and now also with EN certification. As we produce our own tools, assembly facilities and assembly, we are able to reduce turn-around times between order placement and delivery. Everything from a single source! We cover all processes from development to certified assembly. Our clients define the scope of the products and services they choose to acquire. Take advantage of our know-how for your new products. Our experience is a valuable support in developing innovative and cost-effective solutions.

UASystems SA/SKT designed, developed, and produced the SKT helicopter from A to Z. For years SKT has been working closely with UASystems SA (joint venture) for the version SKT UAS-OPH that is currently being worked on, SKT UAS-OPH Optional Piloted Helicopter. SKT has qualified employees in aircraft mechanics. SKT maintains good relationships with suppliers and continuously researches the market to be on the cutting edge of technology. SKT delivers the helicopter ready to fly and with our other partners, the helicopter is converted to SKT UAS-OPH. SKT also offers the helicopter as a 2-seater version on the market. SKT will also assemble and test the eZELOS products in cooperation with our partners.

UASystems

High Efficiency AIR MOBILITY / AIR SURVEILLANCE

Vision Rapid introduction of affordable autonomous air mobility

and air surveillance solutions for the civil and defence sector.

Current Projects UASystems

Market Need

Solution to improve repetitive and/or special missions. Solution to reduce road transportation

• CO2 Emission • Noise • Traffic • Injuries • Investment

Solution to improve / declutter Cities’ Layout.

Solution to increase land & infrastructure security.

VERTICALS TRANSPORT SECURITY &

SURVEILLANCE

DEFENCE

POLICE / TERRITORY SERVICES

AIR-TAXI

LOGISTICS / PORTS / CARGO

OIL & GAS

INFRASTRUCTURE

MANUFACTURING

FARMING / FISHERY / FORREST

UASystems

Product Roadmap

FEATURES

ANTI-JAM HIGH END RADAR

PILOT CAMERA SENSORS

TRANSPORT

Years 2021-22 2024

Piloted Version

2021-23

SKT Skyrider 06

SKT UAS-OPH

SKT UCAS

AP CONTROLLER

AIR CARGO

AIR TAXI

Unmanned Aircraft System - Optionally Piloted Helicopter

AI++ FULL AUTONOMY

Unmanned Cargo Aircraft System

UASystems

Performance

Performance Overview & Specifications: Payload: 300 kg Max. & cont. Horse Power: 170 HP – 150 HP Noise: 73 dB (A) 75m GCS Standard Rugged Portable GCS Data-Link Options MIMO/RF/SATCOM/4+5G Operation Costs per hour: EURO *100-170 *Depending configuration

UAS Unmanned Aircraft Systems OPH Optionally Piloted Helicopter (Manned / Unmanned Version)

SKT UAS-OPH EASA Compliant: EASA Type Certification in progress

UASystems

Performance

Dimension: Overall L 657cm, H 240cm, cabin W & H 130cm - 110cm

SKT UAS-OPH Product Parameters

UASystems

Safety Autopilot MPC

Safety Autopilot MPC Multi Purpose Controller Designed for safety critical aviation application such as OPH,

FBW Fly-by-Wire systems and beyond. Available in single and triple actuator control versions. MPC does fully support DAL-A aspects. (Software DAL

depends on functional criticality). Safety Autopilot Ground Station Ground Station: 3 MPC, displays, indications and remote control

2021/22: Completion of MPC DV testing for UAS-OPH application 2022: Start DV testing in SKT UAS-OPH 2022/23: End DV testing in SKT UAS-OPH 2023 (target): EASA certification testing as UAS-OPH system;

depending on EASA requirements release and EASA availability.

Customized Solution • First EASA approved safety autopilot provider for rotary wing

• Compatible with most mission controller available on the market • No limitation to civil mission avionics • Swiss Production • Dedicated Installation Kit with EASA Form1

Autopilot MPC : in Partnership with Kuerzi Aviation AG

UASystems

Mission Controller

Mission Controller

DO-178C & DO-254, DAL-B compliant Mission design: Configure missions with waypoint definition, payload target definition and coverage analysis. Mission analysis: Rebuild all recorded data from a previous flight and generate plots and reports.

One Click Missions: Through a user-friendly interface, allows operators to program missions (such as mapping, surveillance, delivery…) and execute them doing a single “click”.

Sense & Avoid: Radar, LIDAR or transponder based, permits to perform collaborative and uncollaborated sense and avoid on autonomous missions.

Adaptive control: PID auto-tuning during operation, for platforms with variable plant during the mission such as: fumigation aircrafts, cargo delivery, tethered drone...

Control modes: Fly automatic, fully manual, assisted manual and combined control modes. Selectable at any time during the flight.

Communications: RF, MIMO, SATCOM and 4/5G communications for BVLOS Beyond Visual Line of Sight operations and custom radio modules.

RTK: Positioning: precise positioning up to cm level is possible with the embedded GNSS module, no extra hardware needed.

Dual GNSS: The autopilot embeds dual GNSS for GPS positioning, envying GNSS attitude estimation (no magnetometer needed).

HIGH ACCURACY LANDING IN COMPLEX ENVIRONMENT Integration of redundant flight safety system: LoLaS (Local Landing System), embedded system based on hardware components and their firmware. System providing accurate and reliable positioning information

independent of visibility, weather or environment.

UASystems

COCKPIT HMI OVERVIEW

SKT UAS-OPH UASystems

Power Plant

Ultra Light Engine 4-stroke, 6-cylinder, 3.9L, boxer engine with side valve (flat head) Multi-point fuel injection, supercharched Electronic ignition Liquid cooling Highest quality standards for crankshafts, connecting rods,

camshafts and all engine parts FADEC (Full Authority Digital Engine Control) comprising an

unique 3 ECU Control System for improved redundancy & safety.

European design & manufactured Airworthiness approval: LAS for USA and DULF for Germany Performance: Lightweigth: Installed dry weight (liquids 7kg): 92 kg Silent engines (2.800 RPM) MoGas driven: 20-25 ltrs/hour Power: Max. power 170hp – Continuous power 150hp, nearly flat torque diagram (always the power you need) Compact (LxWxH): 649x 466 x 555 mm TBO: 1’800 hrs

UASystems

Risk Management: Reducing risks, allowing for rapid introduction by improving on proven & certified technologies

BOM Stx / Mech. Sub-Systems

Mechanical Sub-Systems UASystems

SKT Skyrider

Disclosure or duplication without consent is prohibited

Addition Business for Helicopter Schools, Private . . . The Skyrider development was started in December 2011. In June 2013 the company was formed to produce the aircraft and the first production examples were completed in January 2014. The design features a single main rotor and tail rotor, a two-seats-in side-by-side configuration enclosed cockpit with a windshield, skid landing gear and a six-cylinder 3.9L, liquid- cooled, four stroke, supercharged 150 hp piston engine.

Specifications SKT Skyrider General characteristics • Crew: one • Capacity: one passenger • Length: 2.00 m (6.57 ft) • Height: 2.28 m (7 ft 6 in) • Gross weight: 600 kg (1,323 lb) • Fuel capacity: 110 litres (24 imp gal; 29 US gal) • Power plant: 6 cylinder boxer, liquid-cooled, 3.9L, supercharged, 4-stroke (150 hp) • Main rotor area: 38 m2 (410 sq ft)

Performance • Maximum speed: 200 km/h (120 mph, 110 kn) • Cruise speed: 157 km/h (98 mph, 85 kn) • Endurance: 5 hours • Service ceiling: 3,000 m (10,000 ft) • Rate of climb: 7.5 m/s (1,480 ft/min) • Disk loading: 15.7 kg/m2 (3.2 lb/sq ft)

UASystems

Multipurpose UASystems

eZELOS300 UASystems

eZELOS PoC

Specifications eZELOS300:

• Max. Gross Weight: 300kg • Empty Weight: 250kg • Blades: 6 (Coaxial 2 x 3) • Payload: 50kg • Speed: Up to 250km/h • Hover Ceiling: 12.000 feet / 3’650 m (Ground Effect) • Max. Altitude MSL: 19.685 feet / 6’000 m (Electrical) • Operation Costs/Hour: +/- €40 • Range: +750km (Depending Configuration) • Endurance: 30 minutes full electrical. Up to 4 Hours

(Hybrid) Free-Piston Linear Generator • Power: 40kW continuous – 60kW peak • Noise: ≥40-65 dB (A) 75m • Airframe Lenght: 3.50m • Height: 1.50m • Width: 1.20m • Rotor Radius: 3.00m

UASystems

Generator/Range Extender

TODAY TOMORROW

UASystems

Propulsion System

Redundant Electric Engine • eZELOS300 relies on the first electric aircraft engine that can

almost perfectly fulfill the ideal of a fail-safe drive. • Two separate mechanical and electrical motors work without

any gear on one shaft, so that in case of failure of a motor train, the eZELOS300 can make a safety landing.

Generator

Small Battery packs

Lightweight BEETRON Generator • Small, lightweight and powerful with outstanding reliability

and efficiency. • Runs on all liquid and gaseous fuels. • In airport-mode, the aircraft runs on batteries, noiseless

and clean. In long distance flight-mode the low emission and efficient free piston engine can be started. While landing energy can be recuperated.

UASystems

Future eZELOS Air Taxi

Highlights • Coaxial proven technology since 75 years

• High-Speed up to 250Km/h

• Autorotation

• Redundant electro engine

• Revolutionary generator/range extender

• Low noise level

• Very stable and agile even in strong wind

• Less mechanical parts than Multicopter

• Low operating costs

• Long endurance (Generator/Range Extender)

• Aerodynamic frame

• Two passengers one pilot / three passengers (UAS)

• . . .

SAFETY FIRST

UASystems

eZELOS Air-Taxi UASystems

Contact

UASystems SA Unmanned Aircraft Systems

Aéropôle 132

1530 Payerne - Switzerland

+41 76 60 60 842

info@uasystems.com

www.uasystems.com

Member

UASystems