Bayraktar T2. Catalog

INDEX

Letter from the CEO

Subsystems - Avionics - Flight Control Systems

Company Vision

BUK-101 Flight Control Computer

Unmanned Aerial Systems (UAS)

Mission Control Computer

Bayraktar TB2 UAS

KM-301 Magnetometer

Bayraktar TB2 Armed UAS

Mini Autopilot Unit

Bayraktar Mini UAS

BAS-201 Baykar IMU

Air Platforms

BAS-101 Mini IMU

Bayraktar TB2 Tactical UAV

BDS -W-040 Control Surface Rotary Actuator

Bayraktar TB2 Armed Tactical UAV

BLS-B-040 Brake System Linear Actuator

Bayraktar Mini UAV

BDS-208 Dual Redundant Servo Actuator

Payload - Sensor Systems

BDS - 008 Rotary Servo Actuator

Wescam CMX 15D Gimbal Turret

BDS-G-040 Landing Gear Rotary Actuator

BSI-101 Signal Intelligence System

BLS-L-040 Landing Gear Linear Actuator

Payload - Smart Munitions

BLS-T-060 Control Surface Linear Servo Actuator

Roketsan MAM-L

BGKO-101 Power Distribution System

Roketsan MAM-C

ABLi-25 Actively Balanced Lithium Battery System

Ground Control Stations (GCS)

Air Data Recorder

Bayraktar TB2 GCS

Tail Camera

Bayraktar TB2 Mobile GCS

Baykar Bomb Rack Unit

Bayraktar Mini GCS

Mini UAV Data Link

Ground Support Equipment

Bayraktar Digital Video Link

Ground Support Unit

Power Amplifier

Refueling Station

Automatic Tracking Antenna

Mini Mobile Charging Station

Mini Automatic Tracking Antenna

Simulator Systems

Support and Services

101

Bayraktar TB2 HIL Simulator

Staff Training For UAV And Payload Operations

102

C4I Systems

Warranty Policy

103

Operator Interface

Spare Parts

104

Live Video Streaming and Video Archive System

Maintenance Services

104

Geographical Analysis Software

Software Updates

104

Multi-UAV Control & Monitoring Software

Remote Video Terminal System

Wide-Area Mapping Service

To our Esteemed Customers, Partners, and Supporters:

It is with great pleasure that I present yet again a company portfolio that is robust and growing. We have

witnessed in recent past unprecedented achievements in all areas from product development to company

operations to customer delivery and service.

Baykar continues to deliver on its mission to produce the most robust, high-performance unmanned systems not

only in Turkey, but in the world. We have graduated from humble origins as a manufacturer of car parts in the

late 1990s to now delivering industry-grade UAVs that are operational in the field of battle, with over 150,000 flight

hours to boot. In addition to providing surveillance, our systems now deliver smart munitions that have made

our systems a sine qua non in the theater of battle.

Our success is the product of a decade and a half of persistently applying the strongest values of industrial

organization and product development. Our state-of-the-art facility in Istanbul integrates design, prototyping, and

manufacturing under one roof. Our company culture, with its young engineering teams, places a high premium

on combatting hierarchies of position with hierarchies of knowledge and informed judgment. And our product

development integrates multidisciplinary thinking to seamlessly bridge everything from sensor development to

machine learning to platform integration.

We introduce our product portfolio in this catalog for the benefit of our customers. While product improvement

is a never-ending enterprise, we are proud of every system and subsystem delivered - be it large like our TB2,

or small like our sensor kits.

I want to take this opportunity to thank all team members of the Baykar family who have made our extraordinary

journey possible.

Sincereley,

Haluk Bayraktar

CEO, Baykar

VISION

The defense industry is an essential component of the world economy and prime mover in the balance of power

in today’s world. Defense spending has been on the rise due to countries’ attempting to counter the ascendance

of other countries’ weapons technology. This competition has ushered in a technology arms race that, since the

termination of the Cold War, has produced a number of new defense doctrines.

One such doctrine is the importance of “network-centric”, in contrast to “platform-centric” warfare, often considered

the greatest military revolution of the past century. This doctrine stresses the importance of weaning defense

off heavier industries in favor of complete control over information and network management. This shift has

contributed to and benefitted from tidal shifts in economic, trade, and information technology development. As

new information-based economies and technologies have started to supplant older, heavier industry, unmanned

systems in particular started to be seen as a prime opportunity to wean countries off human-intensive operations

on the battlefield. For our country in particular, the shift to unmanned aviation has provided a window of

opportunity not only to bridge the gap between our capabilities and others’ in the world, but also to widen that

gap to our advantage.

Our company draws inspiration from the leadership of technology visionaries from our Republic’s early years

like Nuri Demirağ and Vecihi Hürkuş to build the most advanced technological systems on the global stage by

advancing unmanned aerial systems. In line with their principles, we strive to ensure as independent, Turkey-

centric a technology stack as possible. We further attempt to dovetail emerging high technology with mission-

critical functions to offer our armed forces systems that are reliable, integrated, and complete.

AIR PLATFORM (UAV)

20 21

BAYRAKTAR TB2 TACTICAL UAV

The Bayraktar Tactical Unmanned Aerial System is a medium-altitude, long-endurance class UAS for reconnaissance

Technical Features

operations. With its triple-redundant avionics systems and sensor fusion architecture, it has the capability of fully

autonomous taxi, take off, cruise, landing.

Comm. Range

< 150 km

Fully Automatic Flight System

EO Camera Module

Cruise Speed

70-80 knots

Sensor Fusion Aided Fully Autonomous

IR Camera Module

MORE THAN

Max. Speed

135 knots (110 IAS)

Takeoff and Landing System

Laser Designator

Operational Altitude

22.500 ft

Autonomous Taxi, Parking

Laser Range Finder

60.000 FLIGHT HOURS

Absolute Ceiling

25.000 ft

Semi-autonomous

Laser Pointer

EXPERIENCE

Endurance

< 24 hrs

Fault-tolerant

Wing Span

12 m

Triple Redundant Flight Control System

OPERATIONAL SINCE 2014 WITHIN

Length

6.5 m

Onboard Storage

THE TURKISH ARMED FORCES, GENDARMARIE AND

Takeoff / Landing

Runway (Automatic)

Redundant Servo Actuators

Max Takeoff Weight

650 kg

Redundant Power Architecture

TURKISH POLICE

Payload Capacity

< 55 kg

Fuel Type

Mogas Avgas

NATIONAL ENDURANCE AND ALTITUDE RECORD

100 hp Internal Combustion Engine

Engine Type

(Injection Type, Variable Pitch Propeller)

FOR TURKISH AVIATION

AIR PLATFORM (UAV)

BAYRAKTAR TB2 ARMED TACTICAL UAV

The Armed Bayraktar Tactical Unmanned Aerial System is a medium-altitude, long-endurance-class UAS purposed for

Technical Features

reconnaissance operations. With its triple-redundant avionics systems and sensor fusion architecture, it is capable of fully

autonomous taxi, take off, cruise, landing. The Armed Bayraktar is further capable of delivering up to 4 smart munitions and

Comm. Range

< 150 km

Fully Automatic Flight System

EO Camera Module

precise targetting is available by onboard laser designation. Bayraktar is an all-in-one solution with immediate see-and-hit

Cruise Speed

70 knots

Sensor Fusion Aided Fully Autonomous

IR Camera Module

capability to ensure no collateral damage.

Max. Speed

135 knots (110 IAS)

Takeoff and Landing System

Laser Designator

Operational Altitude

22.500 ft

Autonomous Taxi, Parking

Laser Range Finder

THE ARMED BAYRAKTAR TB2 PROVIDES ARMED

Absolute Ceiling

25.000 ft

Semi-autonomous

Laser Pointer

RECONNAISSANCE, PERSISTENT AIRBORNE

Endurance

< 24 hrs

Fault-tolerant

Wing Span

12 m

Triple Redundant Flight Control System

SURVEILLANCE, AND TARGET ACQUISITION FOR

Length

6.5 m

Onboard Storage

THE TURKISH ARMED FORCES

Takeoff / Landing

Runway (Automatic)

Redundant Servo Actuators

Max Takeoff Weight

650 kg

Redundant Power Architecture

THE TB2 CAN CARRY UP TO

Payload Capacity

55 - 155 kg

Fuel Type

Mogas Avgas

4 SMART MUNITIONS

100 hp Internal Combustion Engine

Engine Type

(Injection Type, Variable Pitch Propeller)

AIR PLATFORM (UAV)

24 25

BAYRAKTAR MINI UAV

The Bayraktar Mini Unmanned Aerial Vehicle System is an intelligent, field-proven robotic

Technical Features

system for short-range reconnaissance applications. The system has been operational since

2007, after having first been deployed within the Turkish Armed Forces.

Comm. Range

< 15 km

Automatic Waypoint Navigation

Cruise Speed

30 knots

Secure Digital Communication

Operational Altitude

2.000 ft

MORE THAN

Home Return and Automatic Landing in Case of

Absolute Ceiling

12.000 ft

Lost Communication

100.000 FLIGHT HOURS

Endurance

60 mins

Smart Battery Management System

EXPERIENCE

Wing Span

2 m

Multi UAV Support

Length

1.2 m

Remote-Range Command / Control And Monitor

TRAINED MORE THAN

Takeoff

Hand Launch

Ground Control Switching

Landing

Parachute / Belly Landing

1.000 OPERATORS

Automatic Takeoff / Automatic Cruise

Operational Temp Range

-20 °C

+55 °C

Automatic Belly Landing / Parachute Deployment

Power

Battery

OPERATIONAL SINCE 2007 WITHIN

Joystick Assisted Semi-Automatic Control

Motor

Electric Motor

THE TURKISH ARMED FORCES, GENDARMARIE, SPECIAL

Stall Control in Case of Electric Motor Disfunction

Payload

2 Axis Day / Termal Camera

Frequency Hopping Spread

Spin Control in Case of Very Harsh Wind Conditions

FORCES, TURKISH POLICE AND QATAR ARMED FORCES

Data Links

Spectrum Digital

PAYLOAD SENSOR SYSTEMS

28 29

WESCAM CMX 15D GIMBAL TURRET

Multi-Sensor Imaging/Lasing Payload Options

Sensors

High Performance Gimbal

Advanced Image Processing

HD thermal, HD daylight and HD low-light cameras

IR Sensor

HD MWIR, 6 FOV

Line-of-sight Stabilization, Typically <5 μradians

Real-time image enhancement on all sensors

Continuous wide-angle zoom

EOW Sensor

8.6-154 mm continuous zoom lens with

Stabilization and Steering (2) Axis Inner (pitch/yaw) (2)

Improved feature recognition and ID

High-magnification step-zoom spotter

2nd gen HD color & VGA low light TV

Axis Outer (azimuth/elevation)

2x, 4x Ezoom

High-sensitivity color low-light imaging

EON Sensor

600/1.000/1.500 mm step zoom lens with

4-axis stabilized turret with internal passive isolator for

Advanced video tracker with automatic target detection

Compact, efficient, reliable laser target designator

3rd gen HD color & (HD low light TV or

excellent stabilization performance

Imaging blending

SWIR camera images designator spot

VGA SWIR)

Sharp optics and excellent stabilization performance

Embedded Moving Target Indication (EMTI)

Laser Designator

100 mJ device @ 1064 nm

results in industry leading target detection, recognition

Image Blending

EO to IR

and identification range performance in the 15” class

Simplified Aircraft Integration

IR Image Processing

6th Gen + auto dead pixel removal +

IMU mounted to optical bench for high target location

false color

accuracy

Electronics unit inside the turret

INS auto-align to aircraft

Built-in vibration isolation

Full laser stabilization minimizes spot jitter

Built-in GPS receiver

PAYLOAD SENSOR SYSTEMS

30 31

BSI-101 SIGNAL INTELLIGENCE SYSTEM

Technical Specifications (Elint)

Frequency Range

10 MHz to 40 GHz

IF Bandwidth

500/100/80/40/20/10/5/1 MHz

ADC Resolution

16 Bits

Frequency Resolution

1 Hz

Frequency Lock Time

50 uS

Dynamic Range

>70 dB

EMI/EMC

Designed to meet MIL-STD-461F

Temperature Range

-40 °C

+85 °C

Baykar’s signal intelligence system BSI-101 is a high performance radio receiver that can be used for airborne

Technical Specifications (Comint)

monitoring and surveillance of the RF spectrum. Based on a software-defined radio architecture, BSI-101 can be

customized to specific needs of ELINT and COMINT systems.

Frequency Range

10 MHz to 6 GHz

Maximum Input Level

+40 dBm (10 Watt)

IF Bandwidth

200/100/80/40/20/10/5/1 MHz

Input Attenuator Range

63.5 dB in steps of 0.25 dB

WITH ITS MINIMAL SWAP, BSI-101 IS WELL-SUITED FOR

ADC Resolution

16 Bits

Spectrum Sweep Rate

30 GHz/s with 12 kHz resolution bandwidth

ADC Sampling Frequency

533.333 MHz

Dynamic Range

>90 dB

DEPLOYMENT ON UAVS AND REMOTELY CONTROLLED

Frequency Resolution

1 Hz

EMI/EMC

Designed to meet MIL-STD-461F

MOBILE GROUND VEHICLES.

Phase Noise

-95dBc/Hz at 100kHz offset

Temperature Range

-40 °C

+75 °C

RF to IF Gain

25 dB

Power Input

12 V, 4 A

AGC Range

50 dB

Weight

< 4 kg

Noise Figure

<5 dB

Monitor Outputs

Video, IF, LO1, LO2

P1dB

>0 dBm

PAYLOAD SMART MUNITIONS

34 35

ROKETSAN MAM-L

ROKETSAN MAM-C

Technical Features

Max. Range (depending on launch altitude and platform velocity)

> 8 km

Max. Range (depending on launch altitude and platform velocity)

> 8 km

Min. Range (depending on launch altitude and platform velocity)

< 2 km

Min. Range (depending on launch altitude and platform velocity)

< 2 km

8 km Range Flight Time

< 80 s

8 km Range Flight Time

< 80 s

Accuracy

< 3 m

Accuracy

< 3 m

Warhead Effectiveness and Targets

ANTI PERSONNEL

Warhead Effectiveness and Targets

ANTI PERSONNEL

Type V Insensitive Munition against bullet impact and fuel fire

Effective in >20 m diameter against personnel

Type V Insensitive Munition against bullet impact and fuel fire

Effective in >20 m diameter against personnel

Type V Insensitive Munition against bullet impact and fuel fire

ANTI ARMOR Battle Tank, armored vehicles (>700 mm RHA armor penetration)

Type V Insensitive Munition against bullet impact and fuel fire

MULTI PURPOSE Armored vehicles (>200 mm), Anti-personnel (>10 m)

Guidance

Inertial Midcourse Navigation + Semi Active Laser (STANAG 3733)

Guidance

Inertial Midcourse Navigation + Semi Active Laser (STANAG 3733)

Weight

21,5 kg

Weight

7 kg

Length

1.000 mm

Length

900 mm

Diameter

160 mm

Diameter

70 mm

GROUND CONTROL STATIONS (GCS)

38 39

BAYRAKTAR TB2 GCS

Baykar designs, develops, and manufactures Command and Control systems and sub-systems such as Shelters,

Interfaces

Features

Consoles, Rack Type Cabinets, Power Distribution Units(PDUs), Monitoring and Command Modules, Command

and Control Software and User Interface Software.

Seperate 220V AC Power Inputs for

Satisfies NATO “6516/SHCPE/86-88” Standards

Generator and Electrical Network

ISO 1161-1976 Compatible Corners

THE GROUND CONTROL STATION IS USED BY THE

External 220V AC Power Output for Ground

STANAG 2338 Compatible Painting

BAYRAKTAR TB2 TACTICAL UAV SYSTEM FOR

Data Terminal

Compatible with EMI and EMC Requirements

External 24V DC Power Input for Redundant

Redundant Power Architecture

THE TURKISH ARMED FORCES AND TURKISH POLICE

Power Source for Critical Hardware

Redundant Pilot and Payload Operator Consoles

C4I Interface

Radio and Intercomm. Systems

Specifications

Ethernet IO Ports

Air Conditioning and NBC Protection Systems

Fiber Optic IO Ports

Lightning Protection Systems

Type

ACE III

Telephone Line IO Ports

Blackout Lamps

Operation Temperature

-40 °C

+60 °C

Monitoring and Command Interface Modules

Sizes

2.240 x 5.900 x 2.300 mm

Command and Control Embedded Software

Weight

2.150 kg

Command, Control and Monitoring Operator Interface Software

GROUND CONTROL STATIONS (GCS)

40 41

BAYRAKTAR TB2 MOBILE GCS

BAYRAKTAR MINI GCS

The Baykar Mobile Ground Control Station is used for operating

Bayraktar TB2 platform far away from main control bases. Its

powerful antennas allow Bayraktar TB2 to take off and land at its

present location and increases its flight range.

The Mobile Ground Control Station consists of a Nato Ace III Shelter,

a hydrolic antenna platform that can be adjusted up to 12m height,

C-Band and UHF antenna systems, and a powerful truck with

hydrolic landing gears that brings mobility to all of these systems.

An indigineous design of Baykar, the Mobile Ground Control Station

has a safe and quick installation by virtue of its sensors and control

valves.

Tower

Vehicle

General Specifications

Features

Hydroulic Control

Total carriage capacity

25 tons

Temperature Range

-30 ºC

+55 ºC

Ruggedized Composite Structure

Adjustable tower operation speed

Range

> 1.000 km

Dimensions

450 x 270 x 53 mm

PC Locking

0-12m height

Weight

3.325 g (±20 g)

System and ATAS Power Switches with Individual Covers

Power

330 PS (243 kW) @ 1.900 d/d

Mechanical safety system

Indicators for System, Internal, External and ATAS Power

Torque

1.300 Nm @ 1.200-1.700 d/d

Electrical Specifications

Flat Keyboard, Capable of Commanding the UAV by the

300 kg weight carriage capacity

Fuel Tank

350 L (Aluminum)

Hardware without PC

Supply Voltage Range

13.5V : 30V DC

Flat Keyboard LED Indicators

External Power Supply

220V AC input, 20V DC output, 160W

Individual Current Protection for ATAS, External Supply and

Battery Supply

Internal Battery Unit

4S, Li-Po, 9Ah

Resettable Fuses

<10 W (Nominal, only Mini GCS)

Power Consumption

Cap Protection for Circular Connectors

<125 W (Maximum, with Mini ATAS and PC)

Easy to Carry

Mighty Mouse Series Circular Connector x4

Connections

(26 Pins x2, 10 pins x1, 6 pins x1)

Communications

Ethernet x2, RS232 x2, CAN x1

GROUND SUPPORT EQUIPMENT

44 45

GROUND SUPPORT UNIT

REFUELING STATION

The Baykar Ground Support Unit (GSU) powers the Bayraktar TB2 Platform on the ground, charges smart batteries, and

The Baykar refueling station is custom-made for the Bayraktar TB2 platform and comes with an 800 litre capacity

provides maintenance via an operator interface. The GSU can charge batteries or the UAV for four hours without needing an

in semi-trailer form factor. The station can both refuel and defuel the aircraft.

external power source. When plugged in, it operates on a standard 220-230V AC source and has wheels for easy mobility.

The station is powered by a 220-230V AC standard ground voltage supplied from the grid or a generator.

Technical Specifications

Interfaces

Capacity

800 L

Operational Temp

-20 °C

+50 °C

Uninterrupted 220V (2A) AC Socket

Dimensions

1.188 x 2.252 x 1.430 mm

Storage Temp

-40 °C

+60 °C

Electrical Network powered 220V (10A) AC Socket

Construction

Semi-Trailer Type

Ethernet IO Port

Working Temperature

-10 °C

+55 °C

RS232 Serial Communication Port

Fuel Pump Output Pressure

1,72 Bar

Refueling Flow Rate

24 L/min

Discharging Flow Rate

17 L/min

Valves

Electro-mechanic

GROUND SUPPORT EQUIPMENT

MINI MOBILE CHARGING STATION

The Mini Mobile Charging Unit is for charging and discharging batteries which are used in the Bayraktar Mini

Unmanned Aerial Vehicle System.

THIS UNIT ENABLES THE CHARGING AND DISCHARGING OF BATTERIES USED IN THE AVIONICS, GROUND

CONTROL STATION AND MOTOR.

Technical Specifications

Electrical Specifications

Operating Temperature

-20 ºC

+55 ºC

Input Voltage

180-264V AC Mains Voltage / 12V DC Voltage

Weight

5.130 g

Charging current capacity

0.1 A-10 A

Sizes

300 x 350 x 150 mm

Discharging current capacity

0.1 A-7 A

Air Cooling

2 Internal Fan (Air Input Channel, Air Output Channel) The ability of driving automatic temperature controlled fan

Power Input Panel Components

Grid Power Connection Connector,

External Cables

Cable that draws power from truck

Grid Power Connection Fuse,

Cable that draws power from regular source on the grid

Grid / Storage Battery Power Source Picking Key,

Cable that connects the battery pack to the charging station

Mobile Charging Station On/Off Switch

Error Notification

Inverse Polarity, Connection Loss, Short Circuit Error,

Connector That Draws Power From Truck

Selection of Wrong Voltage, Low Input Voltage,

Charge Specifications

Charge, Discharge, Balancing

High Input Voltage, Low Cell Voltage,

Charge Capability

Up to 6 cells

High Cell Voltage, Cell Connection Error,

Batteries Charged

Avionic System Battery, GCS Battery,

High Temperature Error

Motor Battery

Internal Balancing Specification

Balancing Mode, Cell balancing during Charge/Discharge

C41 SYSTEMS

OPERATOR INTERFACE

The Baykar Operator Interface (BOI) provides real time control of the UAV and has screens to mon-

itor data coming from the aircraft. Because of its modular structure, BOI is easy to use for a wide

range of operators with different training levels.

Main functions of BOI can be listed as follows

Commands and Controls the UAV

Monitors detailed Telemetry Data

Provides Mission Planning and Mapping functionality

Displays and Configures Camera views

Provides computer-generated graphics for various gauges and displays

Map module of the BOI has the following features

Operator can form flight routes and send them to Autopilot of the UAV.

Operator can display different kinds of map information such as raster map data, shape files and elevation models.

Operator can display ground control stations and ground data terminals on map.

Operator can create airports and also can draw taxi routes for UAV.

Operator can draw different kind of areas such as friendly, fly-restricted etc.

Wide range of elements such as targets, location pins etc. can be added to map by operator.

Main functions of Camera Module are listed below

Display of various types of videos such as Tail Camera videos or Gimbal videos at Operator Interface

Recording of the displayed video

Instant switch between various videos and displaying two video at the same time

Various HUDs (Heads-Up Displays) for different type of missions

C41 SYSTEMS

LIVE VIDEO STREAMING

AND VIDEO ARCHIVE SYSTEM

Broadcast-1

Storage

Media Streaming

Servers

Unit

HIGH

SECURITY

Administrator

NETWORK

Management

Application

Ground Control Station

SYSTEM MAIN FEATURES

Users

Web

UAV

Application

Streams

• Live Video Streaming

• Video Archiving System

Encrypted

• Event Management

WAN Network

Streams

• User Authorization and

Encrypted

Diode

Active Directory Integration

Streams

Solution

Mobil External

Mobil Internal

• Security and Intrusion Prevention

Media Server

Mobile

Media Server

Unidirection Data

Application

Transferring

• Easy and Efficient System Management

Baykar Live Video Streaming System (BLVSS) provides real-time media streaming and archive management solutions

For security of access to live streaming and archived video, the system automatically uses temporary passwords. This

for the defense industry. BLVSS allows many authorized users watch high resolution video streaming in real time with

makes access to the media server more secure. In addition, user name or device id is watermarked on live streaming

low latency. BLVSS consists of a web-based application that allows internal network clients to watch live streams,

and archived videos.

and a mobile application that allows secure streaming of live videos to tablets using mobile networks.

With the mobile solution that can be optionally integrated into the Live Video Streaming System, live streaming can

Live stream videos are recorded in 30-minute-length archive videos. The Comments feature allows users to take

also be watched on mobile devices with Windows platform. Live streams are securely transmitted from high-confidential

notes related to the video streaming. Moreover, users can add tags along with notes and therefore evaluate

networks to mobile devices using end-to-end encryption and unidirectional data transmission (a.k.a. diode).

archived videos with details. These notes can be exported and thus tasks can be scheduled. Archive files can be

searched based on date or metadata.

C41 SYSTEMS

GEOGRAPHICAL ANALYSIS SOFTWARE

Geographic Analysis System (GAS) software developed 100% nationally (fully native resources) by PiriReis Ltd. is a

Main Operations Performed

3-dimensional (3D) virtual globe platform which enables displaying geospatial data compliant to international standards

and analyzing them, on the intranet network of the Turkish Armed Forces.

Near-real-time instant tracking of multiple UAVs.

Instantaneous data interpretation and data compiling

By using the GAS-Unmanned Aerial Vehicle (UAV) Module, developed in cooperation with Baykar and PiriReis, analysis

Displaying UAV’s moving (instant) position and location, field-of-view, foot-

and queries related to UAVs are performed in the operation centers and ground control stations.

(target acquisition, intelligence data collection, digitiz-

print, and trace in 3D environment.

ing, adding notes etc.) from the images captured from

All operations needed to trace and manage UAVs on a 3D virtual globe and make use of the images taken from their

Getting UAV’s information (ID, title, flight altitude, angle, etc.)

camera are performed by using the GAS-UAV. In this way; situational awareness is increased, UAVs are used more

video, with the support of other geospatial data loaded

Viewing UAV’s trace data with its footprint.

effectively and planning and decision-making processes are supported

on the GAS.

Automatic detection and displaying of addresses (city-county-district-street

or place name) of UAV’s location and the target (center of camera view).

Storing snapshot images and trace data of the UAVs in

Viewing meteorological conditions while tracking UAVs.

the database, then querying these data and replaying/

Displaying video coming from UAV’s camera in a separate window.

viewing the selected one.

Taking a snapshot of a frame from the video and positioning this image

on terrain to the true location.

Setting flight route and preparing mission plan for UAVs.

Checking overlapping routes.

Giving a warning when one UAV closes up on another

one or when one UAV comes close to the terrain in a

dangerous way.

C41 SYSTEMS

60 61

REMOTE VIDEO TERMINAL SYSTEM

MULTI UAV CONTROL &

MONITORING SOFTWARE

General Specifications

Details

Central UAV Monitoring System (CMS) is a web based tool that is used for displaying basic information of airborne UAVs

on a single map to users. Thanks to the system, air traffic control, mission planning, antenna and frequency planning

Rugged, portable antenna system enhances EnerLinksIII range

Operating : -20 ºC

+55 ºC

are made easily. CMS allows users to take a general look at all the flights. Location, orientation, remaining fuel, payload

Temperatures

performance.

Non-operating : -40 ºC

+55 ºC

information, emergency situations, communication information (Ground Control Station - GCS, Ground Data Terminal -

Ideal for dismounted on-the-pause applications .

GDT) of the UAVS can be tracked. Additionally, it allows the users to help separation of the UAVS and shows altitude

Backpack Dimensions

99 x 46 x 38 cm

tables, proximity alerts, flight codes, UAV trails. Health status of the ground antennas can be tracked and line-of-sight

Small omni antenna design provides 3dBi of gain.

Antenna Tripod Dimensions

91 cm < height < 183 cm

information can be shown over the map. Permissions can be granted at different levels for users to restrict classified

Wide beamwidth improves usability and allow ease in pointing.

information. CMS is a very useful tool that reflects all the necessary information for the UAV operations with a central

Total Weight

20 kg

Upward-looking antenna for operation at close overhead range.

command.

Fully integrated with all TF components.

Electrical Specifications

The RVT can provide up to five hours of use per mission.

24V with supplied battery pack

The small, light patch antennas provide a wide beam width to

Voltage

or 28V DC

allow easy acquisition and tracking.

Current

Up to 4.0 Amps

The RVT system can provide up to 30 km at 6 Mbps for

Power Consumption

Max 100 W

transmission of high-quality HD video and other sensor data.

2 x 50 OHM SMA Connectors

Connector

and 55-pin Primary Connector

Ethernet Interface

205 cm/81 in

C41 SYSTEMS

WIDE AREA

MAPPING SERVICE

Baykar has available a rapid mapping service to provide orthorectified, color-corrected, high-resolution maps - not just

Example Coverage Patterns (presuming medium flight altitude of 15,000 feet)

photos - overnight. The service can cover hundreds to thousands of square kilometers in one day and deliver the ready-

made map by the next day.

Region

Area (km²)

Example Coverage Time

Resolution (cm/pixel)

The Baykar system is built for rapid development and disassembly, with reliable camera technology. All cameras are

commodity, off-the-shelf cameras and proven to sustain in excess of hundreds of thousands of shots without the need for

San Francisco

130

10 Minutes

replacement. While capture for each flight happens over several hours, the processing of images takes slightly more time

Greater Istanbul

4.000

4.5 Hours

and happens offline.

Adana Fertile Region

10.000

11 Hours

When cruising at TB2 speeds in excess of 200 km / h, this arrangement enables coverage of hundreds of square

(Çukurova)

kilometers per hour, thus enabling entire provinces or even countries to be imaged in one day.

The system includes a web-based application that walks an operator through all phases of map generation, from the

initial designation of the desired area and resolution, to finally image stitching and imagery delivery.

SUBSYSTEMS -

AVIONICS - FLIGHT CONTROL SYSTEMS

BUK-101 FLIGHT CONTROL COMPUTER

Flight control system (FCS) is the most crucial component of a UAV platform which must offer a safe degree of autonomy

combining robust estimation, navigation and control capability. Above all, critical avionic systems have to be continuously

monitored and possible failures must be diagnosed and isolated from the control cycle with immediacy. FCS, developed by

Baykar as part of Turkey’s national UAV initiative, offers a state-of-the-art system which reduces the operator burden while

maximizing safety and reliability. Its triple redundant configuration is the first application on a tactical grade UAV system.

The estimation software included in the flight control system that supplies state information to the control cycles depends

on modern algorithms based on stochastic sensor fusion. Navigation, control and guidance algorithms are capable of fully

autonomous takeoff, landing, taxiing and waypoint navigation.

EMERGENCY SITUATIONS DUE TO SUBSYSTEM

MALFUNCTIONS ARE DETECTED BY A HEALTH-MONITORING

SYSTEM AND SAFE RETURN TO THE BASE IS HANDLED

BY THE AUTOPILOT, RETURNING THE AIRCRAFT ON A

PREDEFINED ROUTE.

Specifications

Features

Supply Voltage

18V - 29V DC

Triple Redundant Main Controller Unit

Power Consumption

Max. 20 W

Triple Redundant System Health Monitoring and Voting Unit

Operating Ambient Temperature

-40 ºC

+55 ºC

Triple Redundant Power Regulating System

Weight

3.060 g

Electrical Isolation Interface

15 RS232, 4 RS422/RS485 Full Duplex,

2 RS422/RS485 Half Duplex,

4 CANBUS Interface

Features

EMI Protection

ESD Protection

Complies with VPX Standards (ANSI/VITA 46.0, 48.0, 48.1, 48.2)

Surge Protection

Lightweight Aluminum Casing

Short Circuit Protection

Vibration Resistant

Reverse Voltage Protection

Conductive Cooling

MIL-DTL-38999 Type Circular Connectors

SUBSYSTEMS - AVIONICS - FLIGHT CONTROL SYSTEMS

KM-301 MAGNETOMETER

MISSION CONTROL COMPUTER

The Auxiliary Mission Computer

controls the non-critical data flow

on the aircraft and transfers data

that can be required by the Flight

Critical Mission Computer. Multiple

communication input/output lanes

provide monitor and control role

of connected avionics and ensures

payload operation and realization of

non-flight-critical functions without

interfering with the main flight control

system.

Specifications

Features

KM-301 is a compact three-axis magnetometer and it can be used as a subsystem with heading output for navigation

systems. Set-Reset capability improves accuracy by eliminating possible strong magnetic disturbances and self-thermal

noise of the sensor.

Input Voltage

18 - 29V DC

Handling of Auxiliary Mission Functions with Safety Microprocessor

Power Consumption

Max. 20 W

Electrical Isolation Interface

15 RS232, 2 RS422/RS485 Full-Duplex,

Operating Temperature

-40 ºC

+55 ºC

2 RS422/RS485 Half-Duplex,

Weight

1,8 kg

4 CANBUS Interface

High Voltage (Surge) Protection

Specifications

Features

Short Circuit Protection

Reverse Voltage Protection

Range

-2 to +2 Gauss

50 Hz Continuous Output.

All Connectors Meets Requirements Specified in MIL-DTL-38999

Operating Temperature

-40 °C

+60 °C

Hard and Soft Magnetic Calibration Adjustment.

Complies with VPX Standards (ANSI/VITA 46.0, 48.0, 48.1, 48.2)

Supply Voltage

18 - 28V DC

Mounting Adjustment using DCM.

Light Weight Aluminum Chassis

Interface

1 x Micro-D (9 pin)

Diagnostic Output for Sensor and Communication Failures.

Vibration Resistant Design

Communication

1 x RS232

Conduction Heat Transfer Structure

SUBSYSTEMS - AVIONICS - FLIGHT CONTROL SYSTEMS

MINI AUTOPILOT UNIT

THIS COMPACT AUTOPILOT SYSTEM CONSISTS OF

DEVELOPED INERTIAL, MAGNETIC, AND PRESSURE

SENSORS AS WELL AS A COMMUNICATION MODEM.

Using an advanced microcontroller with high processor power and advanced stochastic sensor fusion and navigation

algorithms, it provides full automatic departure and landing as well as navigation in autonomous and semi-autonomous

modes. It provides a controlling external input sensor and useful lines with the channels of RS232 and CAN.

Specifications

Features

Operating Temperature

-40 ºC

+55 ºC

Range of measuring ± 10 g

Safety microcontroller which has high processing power.

Weight

158 g

3 Axis Accelerometer

Resolution 0,313 mg

Real Time Operating System.

Sizes

20 × 125 × 90 mm

Noise (RMS) 1 mg

Stochastic state estimation algorithms.

Min. 9V DC

3 Axis Magnetometer

Range of measuring ± 2 Gauss

Developed navigation algorithms.

Voltage

Nominal 12V DC

Micro-D 1/O Connector

Full and semi-autonomous flight modes.

Max. 13,3V DC

External Programming Connector

Automatic route point tracking.

Min. 150 mA

MMCX Telemetry Telecommand RF Connector

Current

Automatic circle tracking.

Max. 230 mA

Full automatic landing and departure.

Avarege Power Dissipation

2,8 W

Range of measuring ± 300 º/s

Emergency monitor, automatic home return in case of emergency.

3 Axis Angular Velocity

Automatic landing with parachute or automatic landing on the body when

Resolution 0.01 °/s

Accelerometer

communication loss occurs.

Noise (RMS) 0.06 °/s

SUBSYSTEMS - AVIONICS - FLIGHT CONTROL SYSTEMS

BAS-201 BAYKAR IMU

BAS-201 is a military grade inertial measurement unit. BIMU - designed, developed and manufactured by Baykar

is used as the primary sensor in sensor fusion and stochastic filtering applications. It is a tactical grade, high

performance unit that provides accurate measurements. Its low size, weight and power consumption makes it a

good choice especially for space constrained applications.

IT IS A TACTICAL GRADE, HIGH PERFORMANCE UNIT

THAT PROVIDES ACCURATE MEASUREMENTS.

Specifications

Accelerometer Specifications

Features

Range

± 5 g

Performance

High Sensitivity Sensors

Precision CNC Machined Aerospace Grade Aluminum Casing

Noise (1σ)

2,5 mg

Operating Temperature

-40 °C…..+55 °C

Bias Over Temperature

±1 mg/°C

Self-Eliminating Any Temperature and Aging Effects

Extended Error Detection & Failsafe Measures

Output Rate

200 Hz

Input Voltage / Power

High Immunity to Shock and Vibration

Applications

Weight

255 g

Unmanned Aerial Systems

Operating Range

15-30V DC

Detailed Diagnostics Data Capability for Testing and Operation

MIL STD 38999,

Connector

Typical Voltage

24/28V DC

Unmanned Ground Vehicles

Series 3 connector, 22 PIN

Redundant Communication With Diverse Interfaces

Typical Current

130 mA

Control and Stabilization

Gyro Specifications

Configurable Communication Protocol for Different Hardware

and Software Applications

Measurement and Testing

Environmental Compatibility (MIL-STD-810F)

Range

± 300 °/s

Wide Operating Temperature Range

High Temperature

Storage / Operation = Method 501.4

Vehicle Health Monitoring

Random Walk

°/√hr

Robotics

Low Temperature

Storage / Operation = Method 502.4

Bias Instability

5 °/√hr

Vibration

Operation / Transportation = Method 514

Bias Over Temperature

± 1 °/s

Humidity

Cycle = Method 507.4

Low Pressure(Altitude)

Storage / Operation = Method 500.4

SUBSYSTEMS - AVIONICS - FLIGHT CONTROL SYSTEMS

BAS-101 MINI IMU

BAS-101 is a military grade inertial measurement unit. Baykar MIMU - designed, developed and manufactured

by Baykar is used as the primary sensor in sensor fusion and stochastic filtering applications. It is a tactical

grade, high performance unit that provides accurate measurements.

ITS LOW SIZE, WEIGHT AND POWER CONSUMPTION

MAKE IT A GOOD CHOICE

Specifications

Features

Applications

Performance

Input Voltage / Power

High Sensitivity Sensors

Unmanned Aerial Systems

Operating Temperature

-40 °C…..+55 °C

Self-Eliminating Any Temperature and Aging Effects

Control and Stabilization

Operating Range

6.5-21V DC (Optional 28V DC)

Output Rate

100 Hz

High Immunity to Shock and Vibration

Measurement and Testing

Typical Current

155 mA @ 12V DC

Weight

61 g

Detailed Diagnostics Data Capability for Testing

Vehicle Health Monitoring

Environmental Compatibility (MIL-STD-810F)

and Operation

Connector

Push-Pull Self-Latching Type

Robotics

High Temperature

Storage / Operation = Method 501.4

Configurable Communication Protocol for Different

Gyro Specifications

Hardware and Software Applications

Range

± 300 °/s

Low Temperature

Storage / Operation = Method 502.4

Wide Operating Temperature Range

Random Walk

°/√hr

Vibration

Operation / Transportation = Method 514

Precision CNC Machined Aerospace Grade

Bias Instability

5 °/hr

Humidity

Cycle = Method 507.4

Aluminum Casing

Bias Over Temperature

± 1 °/s

Extended Error Detection & Failsafe Measures

Low Pressure(Altitude)

Storage / Operation = Method 500.4

Accelerometer Specifications

Electromagnetic Compliance (MIL-STD-461F)

Range

± 5 g

RS103

Radiated Susceptibility / Electric Field

Noise (1σ)

2.5 mg

Bias Over Temperature

±1 mg/°C

RE102

Radiated Emissions / Electric Field

SUBSYSTEMS - AVIONICS - FLIGHT CONTROL SYSTEMS

BDS-W-040 CONTROL SURFACE

ROTARY ACTUATOR

BDS-W-040 Control Surface Rotary Actuator System is

designed and built to meet performance requirements of

modern UAV Flight Control Systems. BDS-W-040 provides

failsafe and jitterless performance with its robust advanced

control system and redundant communication architecture.

Advanced Features

Specifications

Performance

Input Voltage / Power

Dual Redundant Communication via CANbus & RS485

End User Software Parameters

Max. Continous Torque

10.8 Nm

Operating Range

18-28V DC

Gradual Stall for Overload Protection

Dead Band - Null Position - Current Limits

Stall Torque

50.8 Nm

Typical Voltage

24V DC

Brushless Permanent Magnet DC Motor

Temperature Limits - Control Parameters

Nominal Speed

136 °/sec

Standby Current

123 mA

Robust & High Fidelity Controller Design

Detailed Diagnostics Data Output

Max Travel Angle

±120º

Advanced Error Detection & Failsafe Measures

Environmental Compatibility (MIL-STD-810F)

Operating Temperature

-40 °C…..+65 °C

High Power to Weight Performance

Applications

High Temperature

Storage / Operation = Method 501.4

No Load Backlash

<1º

Contactless Shaft Position Sensor

Unmanned Aerial Systems

Low Temperature

Storage / Operation = Method 502.4

Weight

730 g

Precision CNC Machined Aerospace Grade Aliminum Casing

Control Surfaces

Vibration

Operation / Transportation = Method 514

Utility Actuation

Connector

MIL STD 38999

Humidity

Cycle = Method 507.4

Series 3 connector, 19 PIN

Throttle Control

Door

Electromagnetic Compliance (MIL-STD-461F)

Spoiler

RS103

Radiated Susceptibility / Electric Field

RE102

Radiated Emissions / Electric Field

SUBSYSTEMS - AVIONICS - FLIGHT CONTROL SYSTEMS

BLS-B-040 BRAKE SYSTEM

LINEAR ACTUATOR

BLS-B-040 Brake System Linear Actuator System is designed

and built to meet performance requirements of modern

UAV Flight Control Systems. BLS-B-040 provides failsafe

and jitterless performance with its robust, advanced control

system and redundant communication architecture.

Advanced Features

Specifications

Performance

Input Voltage / Power

Dual Redundant Communication via CANbus & RS485

End User Software Parameters

Power

40 W

Operating Range

18-28V DC

Gradual Stall for Overload Protection

Dead Band - Null Position - Current Limits

No Load Feed Velocity

53 mm/sec

Typical Voltage

24V DC

Brushless Permanent Magnet DC Motor

Temperature Limits - Control Parameters

Load Feed Velocity

43 mm/sec

Standby Current

123 mA

Robust & High Fidelity Controller Design

Detailed Diagnostics Data Output

Max. Continuous Force

410 N

Environmental Compatibility (MIL-STD-810F)

Advanced Error Detection & Failsafe Measures

Max. Force

2,180 N

High Temperature

Storage / Operation = Method 501.4

High Power to Weight Performance

Applications

Operating Temperature

-40 °C.….+65 °C

Low Temperature

Storage / Operation = Method 502.4

Contactless Shaft Position Sensor

Unmanned Aerial Systems

Weight

864 g

Vibration

Operation / Transportation = Method 514

Precision CNC Machined Aerospace Grade Aliminum Casing

Control Surfaces

Humidity

Cycle = Method 507.4

Utility Actuation

MIL STD 38999

Connector

Series 3 connector, 19 PIN

Electromagnetic Compliance (MIL-STD-461F)

Throttle Control

Door

RS103

Radiated Susceptibility / Electric Field

Spoiler

RE102

Radiated Emissions / Electric Field

SUBSYSTEMS - AVIONICS - FLIGHT CONTROL SYSTEMS

BDS-208 DUAL REDUNDANT

SERVO ACTUATOR

BDS-208 Dual Redundant Servo Actuator System is designed

and built to meet performance requirements of modern UAV

Flight Control Systems. BDS-208 provides failsafe and jitterless

performance with its robust advanced control system and

redundant communication architecture.

Advanced Features

Specifications

Performance

Input Voltage / Power

Dual Redundant Communication via CANbus & RS485

End User Software Parameters

Power

80 W

Operating Range

18-28V DC

Gradual Stall for Overload Protection

Dead Band - Null Position - Current Limits

Nominal Speed

132 °/sec

Typical Voltage

24V DC

Brushless Permanent Magnet DC Motor

Temperature Limits - Control Parameters

Max. Continuous Torque

1,3 Nm

Standby Current

70 mA

Robust & High Fidelity Controller Design

Detailed Diagnostics Data Output

Max. Torque

3,5 Nm

Environmental Compatibility (MIL-STD-810F)

Advanced Error Detection & Failsafe Measures

Operating Temperature

-40 °C.….+65 °C

High Temperature

Storage / Operation = Method 501.4

High Power to Weight Performance

Applications

Weight

670 g

Low Temperature

Storage / Operation = Method 502.4

Contactless Shaft Position Sensor

Unmanned Aerial Systems

Vibration

Operation / Transportation = Method 514

Precision CNC Machined Aerospace Grade Aliminum Casing

Control Surfaces

MIL STD 38999

Connector

Series 3 connector, 19 PIN

Humidity

Cycle = Method 507.4

Utility Actuation

Electromagnetic Compliance (MIL-STD-461F)

Throttle Control

Door

RS103

Radiated Susceptibility / Electric Field

Spoiler

RE102

Radiated Emissions / Electric Field

SUBSYSTEMS - AVIONICS - FLIGHT CONTROL SYSTEMS

BDS-008 ROTARY

SERVO ACTUATOR

BDS-008 Rotary Servo Actuator System is designed and

built to meet performance requirements of modern UAV

Flight Control Systems. BDS-008 provides failsafe and

jitterless performance with its robust advanced control

system and redundant communication architecture.

Advanced Features

Specifications

Performance

Input Voltage / Power

Dual Redundant Communication via CANbus & RS485

End User Software Parameters

Power

8.0 W

Operating Range

18-28V DC

Gradual Stall for Overload Protection

Dead Band - Null Position - Current Limits

Nominal Speed

132 °/sec

Typical Voltage

24V DC

Brushless Permanent Magnet DC Motor

Temperature Limits - Control Parameters

Max. Continuous Torque

1,3 Nm

Standby Current

70 mA

Robust & High Fidelity Controller Design

Detailed Diagnostics Data Output

Max. Torque

3,5 Nm

Advanced Error Detection & Failsafe Measures

Environmental Compatibility (MIL-STD-810F)

Operating Temperature

-40 °C.….+65 °C

High Power to Weight Performance

Applications

High Temperature

Storage / Operation = Method 501.4

Weight

0,341 kg

Contactless Shaft Position Sensor

Unmanned Aerial Systems

Low Temperature

Storage / Operation = Method 502.4

Precision CNC Machined Aerospace Grade Aliminum Casing

Control Surfaces

MIL STD 38999

Connector

Vibration

Operation / Transportation = Method 514

Series 3 connector, 19 PIN

Utility Actuation

Humidity

Cycle = Method 507.4

Throttle Control

Door

Electromagnetic Compliance (MIL-STD-461F)

Spoiler

RS103

Radiated Susceptibility / Electric Field

RE102

Radiated Emissions / Electric Field

SUBSYSTEMS - AVIONICS - FLIGHT CONTROL SYSTEMS

BDS-G-040 LANDING GEAR

ROTARY ACTUATOR

BDS-G-040 Landing Gear Rotary Actautor System is designed

and built to match performance characteristics of modern

UAV Flight Control Systems. BDS-G-040 provides failsafe and

jitterless performance with its robust advanced control system

and redundant communication architecture.

Advanced Features

Specifications

Performance

Input Voltage / Power

Dual Redundant Communication via CANbus & RS485

End User Software Parameters

Maximum Torque

12 Nm

Operating Range

18-28V DC

Gradual Stall for Overload Protection

Dead Band - Null Position - Current Limits

Max. Continous Torque

10,8 Nm

Typical Voltage

24V DC

Brushless Permanent Magnet DC Motor

Temperature Limits - Control Parameters

Stall Torque

40 Nm

Standby Current

70 mA

Robust & High Fidelity Controller Design

Detailed Diagnostics Data Output

Nominal Speed

95 °/ sec

Advanced Error Detection & Failsafe Measures

Environmental Compatibility (MIL-STD-810F)

Max Travel Angle

±120°

High Power to Weight Performance

Applications

High Temperature

Storage / Operation = Method 501.4

Operating Temperature

-40 °C…..+65 °C

Contactless Shaft Position Sensor

Unmanned Aerial Systems

Low Temperature

Storage / Operation = Method 502.4

No Load Backlash

<1º

Precision CNC Machined Aerospace Grade Aliminum Casing

Control Surfaces

Vibration

Operation / Transportation = Method 514

Weight

730 g

Utility Actuation

Humidity

Cycle = Method 507.4

Throttle Control

MIL STD 38999

Connector

Series 3 connector, 19 PIN

Door

Electromagnetic Compliance (MIL-STD-461F)

Spoiler

RS103

Radiated Susceptibility / Electric Field

RE102

Radiated Emissions / Electric Field

SUBSYSTEMS - AVIONICS - FLIGHT CONTROL SYSTEMS

BLS-L-040 LANDING GEAR

LINEAR ACTUATOR

BLS-L-040 Landing Gear Linear Actuator System is designed

and built to meet performance requirements of modern

UAV Flight Control Systems. BLS-L-040 provides failsafe and

jitterless performance with its robust advanced control system

and redundant communication architecture.

Advanced Features

Specifications

Performance

Input Voltage / Power

Dual Redundant Communication via CANbus & RS485

End User Software Parameters

Power

40 W

Operating Range

18-28V DC

Gradual Stall for Overload Protection

Dead Band - Null Position - Current Limits

No Load Feed Velocity

22 mm/sec

Typical Voltage

24V DC

Brushless Permanent Magnet DC Motor

Temperature Limits - Control Parameters

Load Feed Velocity

18 mm/sec

Standby Current

123 mA

Robust & High Fidelity Controller Design

Detailed Diagnostics Data Output

Max. Continuous Force

461 N

Environmental Compatibility (MIL-STD-810F)

Advanced Error Detection & Failsafe Measures

Max. Force

2.463 N

High Temperature

Storage / Operation = Method 501.4

High Power to Weight Performance

Applications

Operating Temperature

-40 °C.….+65 °C

Low Temperature

Storage / Operation = Method 502.4

Contactless Shaft Position Sensor

Unmanned Aerial Systems

Weight

707 g

Vibration

Operation / Transportation = Method 514

Precision CNC Machined Aerospace Grade Aliminum Casing

Control Surfaces

MIL STD 38999

Humidity

Cycle = Method 507.4

Utility Actuation

Connector

Series 3 connector, 19 PIN

Electromagnetic Compliance (MIL-STD-461F)

Throttle Control

Door

RS103

Radiated Susceptibility / Electric Field

Spoiler

RE102

Radiated Emissions / Electric Field

SUBSYSTEMS - AVIONICS - FLIGHT CONTROL SYSTEMS

BLS-T-060 CONTROL SURFACE

LINEAR SERVO ACTUATOR

BLS-T-060 Control Surface Linear Servo Actuator System

is designed and built to meet performance requirements

of modern UAV Flight Control Systems. BLS-T-060 provides

failsafe and jitterless performance with its robust advanced

control system and redundant communication architecture.

Advanced Features

Specifications

Performance

Input Voltage / Power

Dual Redundant Communication via CANbus & RS485

End User Software Parameters

Power

60 W

Operating Range

18-28V DC

Gradual Stall for Overload Protection

Dead Band - Null Position - Current Limits

No Load Feed Velocity

84 mm/sec

Typical Voltage

24V DC

Brushless Permanent Magnet DC Motor

Temperature Limits - Control Parameters

Load Feed Velocity

73 mm/sec

Standby Current

191 mA

Robust & High Fidelity Controller Design

Detailed Diagnostics Data Output

Max. Continuous Force

523 N

Advanced Error Detection & Failsafe Measures

Environmental Compatibility (MIL-STD-810F)

Max. Force

3,293 N

High Power to Weight Performance

Applications

High Temperature

Storage / Operation = Method 501.4

Operating Temperature

-40 °C…..+65 °C

Contactless Shaft Position Sensor

Unmanned Aerial Systems

Low Temperature

Storage / Operation = Method 502.4

Weight

0,844 kg

Precision CNC Machined Aerospace Grade Aliminum Casing

Control Surfaces

Vibration

Operation / Transportation = Method 514

MIL STD 38999

Utility Actuation

Connector

Humidity

Cycle = Method 507.4

Series 3 connector, 19 PIN

Throttle Control

Door

Electromagnetic Compliance (MIL-STD-461F)

Spoiler

RS103

Radiated Susceptibility / Electric Field

RE102

Radiated Emissions / Electric Field

SUBSYSTEMS - AVIONICS - FLIGHT CONTROL SYSTEMS

90 91

BGKO-101

ABLi-25

POWER DISTRIBUTION

ACTIVELY BALANCED

SYSTEM

LITHIUM BATTERY

BGKO-101 Power Distribution Unit is a military grade avionic - designed,

SYSTEM

developed and manufactured by Baykar that supplies power to all

other avionics and checks their status, controls alternators and batteries

The actively balanced Lithium based smart battery unit is the

as well. The unit has a redundant control architecture that is designed

lightest weight & highest energy level battery pack designed for

with safety microprocessors. Moreover, the system monitors the health

Unmanned Applications. The system is built to military standards

of the power distribution, takes protective measures for faults and

and has special protective measures to ensure reliability and

presents detailed diagnostic data to the flight control system.

performance.

Technical Specifications

Features

Technical Specifications

Features

Voltage

18-29 V DC

Redundant control circuit and power distribution of flight and mission critical system

Capacity

20 Ah

Carbon case and aluminum base

Redundant communication system

Lightweight box structure

Protection

Over Voltage Protection (OVP)

Voltage

Min 18V DC

Original battery charging system over alternator

Heat isolation layers for cells

Over Current Protection (OCP)

Normal 22,2V DC

Detailed power status fault log for all avionics

Evacuation hole for pressure security

ESD, EMI, EMC Protection

Max 25,2V DC

Power supply to more than 50 avionics. Monitoring of voltage, current and circuit breaker status

24V DC and 12V DC Outputs

Number of Power Distributed Unit

> 50

Power critical mode (switch off all non-flight-critical units)

Current

Charge 40 A

Blade type fuse holder at external 24V and 12V output terminal

Distributed Total Power

> 2.000 W

Detailed list of battery and alternator faults

Suitable endings for ring tongue terminals

Discharge 100 A

Communication

RS232, CAN

MIL-PRF-6106, MS 27742, MIL-R-83536 standart power switching components

MIL-DTL-38999 type control connector

Instant Discharge 200 A (<10 s)

Standarts of Switching Component

MIL-PRF-6106

MIL-DTL-38999, MIL-C-5015 standart connectors

Internal battery control unit

Nominal Current

Charge 10 A

Alternator control

Capability to increase capacity by heating cells in cold weathers

MS 27742

Smart battery control

Discharge 10 A

Internal active balancing system

MIL-R-83536

Fault control

5 level battery indicator and error indicator on battery box

Storage Temperature

-10 °C

40 °C

Standarts of FUSE Component

MS 3320

Voltage regulation

Button activated LED indicator

Recommended 25 °C (±3 °C)

Connectors

MIL-DTL-38999

Temperature control

2 open-collector pins on the circular connector for external LED indicator

MIL-C-5015

Cell Arrangement

6S-1P

Redundant communication - Dual CAN

Operating Temperature

-40 °C

+60 °C

Weight

4.300 g

Individual temperature sensors for battery cells and control circuit

SUBSYSTEMS - AVIONICS - FLIGHT CONTROL SYSTEMS

AIR DATA RECORDER

TAIL CAMERA

BAYKAR BOMB RACK UNIT

Air Data Recorder is a unit that is capable of recording an analog

Tail Camera is an analog output PAL system camera

video input and one serial port data with AES-256 encryption. The

with a wide angle of view for aerial applications.

Baykar Bomb Rack Unit has been developed in MIL-STD-8591 and MIL-STD-

unit has a rugged frame that can operate in a broad temperature

Heated lens allows a clear view in humid conditions.

1760E standards for arming the tactical UAVs. Aluminum alloys are extensively

range. Small size and lightweight structure with solid state component

used in production. Military standard connectors are used on uniquely designed

architecture offers an excellent solution for UAV systems.

control board and store interface connectors.

Store interface connector can be mounted to two different points if needed.

Different types of sway braces can be used for various munitions.

Safety and ease of use is in foreground in the design. Armament can be easily

done by using arming knob on the system. On the cruise, system remains in

safety lock mode both electrically and mechanically. On the ground, in case,

system can be disarmed via onboard manual release mechanism.

A VERY LIGHT SOLUTION FOR THE

SMART MICRO MUNITIONS!

Advanced Specifications

Mechanical Adjustment for Field of View Orientation

100 Hours of Analog Video Recording

Technical Specifications

Heated Lens for Fog Protection

AES-256 Encrypted Logging of Serial Port Input

Replaying while Recording

Design Standard

MIL-STD-8591 and MIL-STD-1760E

Fast Forward and Rewind

Hook Class

100 lb

Flight Metadata Recording on Video Data

Dimensions

106 x 208 x 103 mm

Weight

~1.000 g

Technical Specifications

Construction

Aluminum

Operating Temperature

-40 °C

+55 °C

Horizontal FOV

140°

Working Temperature

-40 °C - +60 °C

Supply Voltage

18 - 28V DC

Operating Temperature

-40 °C

+60 °C

Platform Interface Connectors

MIL-C-38999 Referred

Power Consumption

60 W max.

Supply Voltage

18 - 28V DC

Store Interface Connector

Spring Contact, EMI protected

Interface

2xMighty Mouse Series Connector (13 and 19 pin)

Interface

1 x Mini BNC (Analog Video)

1 x Circular Power Connector

Communication

1 x RS232 for Data Recording

1 x RS232 for Diagnostics and Control

1 x 10/100/1000 Mbit Ethernet

SUBSYSTEMS - AVIONICS - FLIGHT CONTROL SYSTEMS

MINI UAV

VIDEO LINK

Bayraktar Mini UAV Video Link is an analog video and audio transceiver designed for harsh environments.

It is ideal for law enforcement, surveillance and other applications requiring high sensitivity video and audio

transmission in a compact package.

Technical Specifications

RF Characteristics

Frequency Bands

L, S or C Band

Applications

Frequency Selection

Full Band Channelized or Up To 16 Fixed Channels

Real-Time Video Surveillance

Frequency Stability

±5 ppm

Law Enforcement

Sensitivity

-90 dBm

UAVs and UGVs

RF lnput impedance

50 Ohm Nominal, VSWR 2:1 Maximum

Covert wireless video and audio transmission

Advanced Features

Complete Fm Video/Audio Transceiver System

Video & Audio Characteristics

Mechanical

No Latency Reception With Excellent Sensitivity

Modulation Type

Analog FM

Material

CNC Machined T6061-T6 Aluminum

Transmission of Analog Audio and Video Over Distances Up To 32 Km (20 Mi)

Video Standard

NTSC, PAL or SECAM

Finish

Nickel Plated or Gold lridite

Operation In L, S or C Bands at Factory-Preset or User-Selectable Frequencies

Video Output lmpedance

75 Ohm Nominal

Dimensions

86 x 81.5 x 17 mm

Remote Control Via Rs232

Video Output Level

1 Vpp (typical)

Weight

135 g

Crystal Clear Video Output Independent of the Video Format (Ntsc, Pal or Secam)

Video SNR

40 dB (typical)

RF Output Connector

SMA Female

Stereo Audio Output

Audio Output Level

3 Vpp (Max)

Extremely Compact and Rugged Package (86X81,5xl7mm)

Audio Output lmpedance

10 kOhm (typical)

Environmental

Weight 135 g

Audio SNR

50 dB (typical)

Operating Temperature

-40 °C

+55 °C

Proven Track Record

Audio Frequency Response

50 Hz to 15 kHz (typical)

Humidity

Up to 95%

Input Voltage

8V to 20V DC Reverse Polarity Protected

Fiber Glass Radome Structure

Current Draw (Typical at 12V)

200 mA (typical)

SUBSYSTEMS - AVIONICS - FLIGHT CONTROL SYSTEMS

BAYRAKTAR DIGITAL VIDEO LINK

POWER AMPLIFIER

The Bayraktar digital video link is low-cost and low-swap video transmission and reception system for Intelligence, Surveillance and

Reconnaissance (ISR) applications. It features dual H.264 compression engines capable of encoding HD and SD videos up to 1080p

resolution. In addition to dual integrated H.264 compression, input video decoding of HD-SDI and analog video are performed on-board.

As a complete end-to-end solution, Baykar’s digital video link system requires no additional hardware for deployment.

Application Areas

Airborne ISR

IP video surveillance

Technical Specifications

Transmitter Unit (TX)

Receiver Unit (RX)

Low EVM

<3 % for QAM64

Up to 150 km LOS range with Bayraktar

RF to ethernet based receiver unit

Adjustable output power

+20 to +43 dBm

Digital RX and PA

Integrated LNA (0.56dB NF)

Good efficiency

45 W consumption @ 10 W RF output

Simultaneous transmission of 1 HD and 1

1080p30, 1080p25,

Integrated isolator

SD video

Various video formats

1080i60, 720p60, PAL,

Compact and rugged package

QPSK, QAM16 and

NTSC

Selectable modulation

Size

124 x 131 x 75 mm

QAM64

Size

119 x 118 x 40 mm

Weight

650 g

L, S or C Band

Weight

320 g

Operation temp range

-40 °C

+55 °C

Low power consumption

Operation temp range

-40 °C

+60 °C

On-board HD SDI and analog decoding

On-board dual H.264 encoders

Size

136.6 x 118 x 52 mm

Weight

326 g

Operation temp range

-40 °C

+65 °C

SUBSYSTEMS - AVIONICS - FLIGHT CONTROL SYSTEMS

98 99

AUTOMATIC

MINI AUTOMATIC

TRACKING ANTENNA

Automatic Tracking Antenna System (ATAS) provides a complete and

Mini Automatic Tracking Antenna System (Mini ATAS) is a unit that provides

highly efficient ground station solution between the ground and air

video, telemetry and telecommunication between the UAV and the Ground

for the transmission of UAV video and other data. A primary objective

Control Station by pointing the ground data terminal to the mini UAV

of the antenna is to ensure transmitted data is never lost. This dual-

automatically. It consists of an automatic pointing antenna system, an

axis auto-tracking antenna has up to 150 km signal range. Antennas

ATAS control unit, a tracking mechanism, a tracking antenna cable set, a

can automatically locate the RF, GPS or telemetry signals and track

telemetry and telecommunications antenna, video receiver antenna and

them quickly. All major elements are housed inside the radome.

several feet of cabling.

Components are transported seperately into the field and the system

is easily and quickly assembled.

Interior Equipments

Operating Temperature -30 C°

+55 C°

Physical Specifications

Sizes 741 X 1.062 X 185 mm

Total Weight 9.320 g

Technical Specifications

Tripod Specifications

Technical Specifications

Power

Input/Output

+/- 200 degrees Azimuth Axis Rotation

Tripod, Elevator Column

Voltage

12V DC Min

26 Pin Mighty Mouse Series

+90/-10 degrees Elevation Axis Rotation

Load Capacity

90 kg/200 lbs

Connector

16V DC Nominal

60°/sec Azimuth Angular Speed

Max. Height

215 cm/85 in

1 unit Ethernet bus

24V DC Max

45°/sec Elevation Axis Rotation

Min. Height

105 cm/41,5 in

Radio Sensitivity

-108 dBm

Current Value

1,2 A Nominal

12.9 Nm Azimuth Torque Capacity

Weight

19,1 kg/42 lbs

Output Power

1 W

Power Dissipation

20 W

17.2 Nm Elevation Torque Capacity

Maximum Spread Diameter

205 cm/81 in

Mechanical Limits in Azimuth and Elevation Axises

Column Travel

45 cm/18 in

Internal Sensors

Mechanics

Self-Locking Gear Set in Azimuth and Elevation Mechanism

Transport dimension

17,5 x 49,5 (44 x 124)

GNSS Receiver

360 degree infinite tracking

Water Proof

GPS, GLONASS

Sewing from +90 to -10 degrees

Weight : 32,3 kg

Horizontal Position Sensitivity

2,5 m (CEP % 50, 24 hour Statik)

3-level adjustable height mounting feet

CNC Machined Aluminum Structure

Initial resolution time

26 s

Easy installation for antenna and system connections

Fiber Glass Radome Structure

3 Axis Magnetometer

-40 °C

+55 °C Operating Temperature

Range of measuring

±2 Gauss

102 103

STAFF TRAINING FOR UAV AND

SPARE PARTS

PAYLOAD OPERATIONS

Availability of spare parts for both scheduled and unscheduled maintenance operations critically affect operational readiness

of the sytems. For successful UAV operations, Baykar deploys field depots at Client bases. Scheduled maintenance spare

Baykar provides two types of training programs for our Clients’ technical staff. All training programs are provided by Baykar at

parts are planned and transferred to these depots. For quick fixes and unscheduled maintenance works, an inventory of

its Kesan facility - having its own UAV fleet and runway. Trainings are conducted in two phases, namely theoretical/system and

critical parts are kept at these depots. Through years of operational usage experience, additional critical parts like avionics

applied trainings. The TB2 UAS curriculum includes a one week introduction, followed by three to four weeks of theoretical and

and engine components are also stored in these depots to increase part and component availability.

system trainings, and seven to eight weeks of flight simulations, payload operator flight trainings and applied flight trainings. The

MINI UAS curriculum includes four weeks of theoretical and system trainings followed by five weeks of flight simulations and

applied flight trainings. During the applied flight trainings, pilot candidates actually fly Baykar’s TB2 and MINI UAVs.

UPON THE COMPLETION OF TRAINING, EVALUATION

MAINTENANCE SERVICES

EXAMS ARE CONDUCTED FOR EACH TRAINING MODULE

AND SUCCESSFUL CANDIDATES ARE AWARDED THEIR UAS

TRAINING CERTIFICATES.

Baykar’s maintenance policy is to assist and support its Clients to get the most out of their UAV systems. To keep

UAVs operational most of the times, Baykar provides technical support to Client technical staff for repairs and

maintenance works at line level; and carries out 1000 flight hr major overhauls with its own staff.

Baykar monitors and proactively plans major overhaul needs of its Clients in order to improve operational readiness

of the systems and minimize downtime. Scheduled maintenance is planned beforehand and required parts and

WARRANTY POLICY

technical staff is deployed before the overhaul time is reached.

Our Clients benefit from system-level warranty for each delivered system and is applicable.

The warranty period commences with the delivery of UAS and is valid for the following durations per each system:

• For TB2 UAS, 2 calendar years or 4000 flight hours, whichever is reached first

• For MINI UAS, 2 calendar years or 600 flight hours, whichever is reached first.

SOFTWARE UPDATES

WARRANTY PACKAGE INCLUDES TECHNICAL SUPPORT

Embedded system and user interfaces of the components are updated in order to meet Clients’ demands and

DURING THE WARRANTY PERIOD AND FOR TB2 PLATFORMS,

operational requirements. Critical updates are scheduled with immediate action to keep the system availability at

IT ADDITIONALLY COVERS MAJOR OVERHAULS AT EVERY

its maximum.

1000 FLIGHT HOURS.

After the system warranty period ends, maintenance and repairs are handled as per component-based warranty.

UNMANNED AEA IAL SYSTEMS

BAYKAR

The Bayraktar Tactical Unmanned Aerial

MORE THAN

System is a medium-altitude, long-endurance

130,000 FLIGHT HOURS

class LJAS for reconnaissance operations. With

its triple-redundant avionics system and sensor

EXPERIENCE

fusion architecture, it has the capability of fully

autonomous taxi, take off, cruise and landing.

OPERATIONAL

The Bayraktar Armed UAV has a standalone

SINCE 201L1 WITHIN

precise see, designate and hit capability with

THE TURKISH ARMED

its L MAM-L or MAM-C guided bombs and

onboard designator. The system offers an

FORCES, GENDARMARIE

all-in-one solution with an easy to operate and

AND TURKISH POLICE

maintain airframe which reduces operational

TECHNCAL. SPECIFICATIONS

TES..:1-INICAL CAPABILITIES

necessities and cost.

Comm. Range

> 150 km

Fully Automatic Flight System

NATIONAL ENDURANCE

Cruise Speed

70 knots

Sensor Fusion Aided Precise Take-oft

and Landing System

AND ALTITUDE RECORDS

Max. Speed

116 KTAS

@ 16,000 ft

Autonomous Taxi

Operational Alliflude

18,000 ft

Semi-Autonomous

FOR TURKISH AVIATION

Absolute Ceiling

25,000 ft

Fault-Tolerant System Achitecture

Endurance

>24 hrs

Triple Redundant Flight Control System

Wing Span

Redundant Servo Actuators

Length

6.5 m

Redundant Electrical Power Architecture

Takeoff / Landing

Runway (Automatic)

EC Camera Module

Max Takeoff Weight

650 kg

IR Camera Module

Payload Capacity

55 kg Gimbal Camera • 85 kg Ext. Store

Laser Designator

Fuel Capacity / Type

Mogas / Avgas

Laser Range Finder

Engine Type

100 lip Internal Combustion Engine

(Injection Type, Variable Pitch Propeller)

Laser Pointer