Avionics/Subsystems

The Mini Autopilot Unit (MAU) uses a high-power microprocessor, integrated sensors and advanced stochastic sensor fusion and navigation algorithms for accurate status estimation.  This unit allows fully automatic descent and take-off in autonomous and semi-autonomous modes.  In addition, it can control external sensors and provides available external communication channels like RS232 and CAN-Bus. 

Operating Temperature: -40 ºC ..... + 55 ºC
Weight: 158 gr
Dimensions: 20 mm (E) × 125 mm (B) × 90 mm (H)
 

The BAS-101 is a military grade inertia measuring unit. The Baykar Mini IMU is designed, developed and produced by Baykar and used as the primary sensor in its sensor fusion and stochastic filtering applications. The Baykar Mini IMU tactical class is a high performance inertial measuring unit that provides precise measurement.

Operating Temperature: -40 ° C….. + 55 ° C
Output Frequency: 100 Hz
Weight: 61 g

Lithium Smart Battery Unit comes with active balancing and a very lightweight and high-energy capacity profile  designed specifically for unmanned applications. 
It is designed according to specifications and has special protection notifications to ensure reliability and performance.

Capacity: 20 Ah
Voltage: Minimum 18V DC, Rated 22.2V DC, Maximum 25.2V DC
Storage Temperature: -10 ° C ..... 40 ° C
Weight: 4,300 g
 

The BAS-201 is a military-grade inertial measuring unit. Designed, developed and manufactured by Baykar, the BIMU is used as the primary sensor in sensor fusion and stochastic filtering applications. This tactical class, high performance product provides accurate measurements. With its small size, light weight and low power consumption, this product stands out as a good choice especially for applications with limited volume.

Operating Temperature: -40 ° C… .. + 55 ° C
Output Frequency: 200 Hz

The Power Distribution Unit is a military-grade avionics system designed, developed and manufactured by Baykar for the purpose of powering avionics in the aircraft and controlling their status, alternators and batteries. The unit has a redundant control architecture designed with secure microprocessors. In addition, the system monitors its power distribution, checks its status, takes preventive measures in case of failure, and transfers detailed diagnostic data to the flight control system.

Voltage Range: 18-29V DC
Number of Units Feeded> 50
Total Distributable Power> 2,000 W
Communication: RS232, CAN
Operating Temperature: -40 ° C ..... + 60 ° C

The Air Data Recorder is capable of recording analog video data and data transmitted through a serial communication port using the AES-256 encryption method. This unit has a recessed frame structure that allows it to operate in a wide temperature range. The small size and light weight combined with the solid state architecture make it the perfect solution for UAV systems.

Operating Temperature: -40 ° C ..... + 55 ° C
Supply Voltage: 18 - 28 VDC
Power Consumption Max: 60 W

The tail camera is a PAL system camera with analog output and wide viewing angle for aviation applications. Heated lenses provide clear vision even in humid environments.

Operating Temperature: -40 ° C ..... + 60 ° C
Supply Voltage: 18 - 28V DC
Interface: 1 x Mini BNC (Analog Video)
1 x Circular Power Connector

The mission critical computer controls non-critical data flow in the aircraft and transfers any data required by the Flight Control Computer. Multiple communication input / output channels allow monitoring and control of avionics connected to it. It also provides useful payload and the implementation of non-flight critical functions without interfering with the main flight control system.

Input Voltage: 18V - 29V DC
Max Power Consumption: Max. 20 W
Operating Temperature: -40 ºC ..... + 55 ºC
Weight: 1.8 kg

The Flight Control Computer is the most important component of aircraft that should provide a reliable level of autonomy with proper forecasting, navigation and control capability. In particular, all critical avionic systems must be continuously monitored and potential faults must be identified and immediately isolated from the control loop.  Its triple redundant system is a first for tactical class UAVs. The forecasting software within the UKS, which sends status information to the control loop, employs high-level stochastic sensor fusion. Navigation, control and orientation algorithms are fully capable of autonomous departure, landing, taxi and route tracking.

Supply Voltage: 18V - 29 VDC
Max Power Consumption: 20W
Operating Ambient Temperature: -40 ºC ..... + 55 ºC
Weight: 3.060 gr

The Control Surface Linear Servo Actuator System is designed and manufactured to meet the performance requirements of modern UAV Flight Control Systems. The BLS-T-060 provides fail-safe and vibration-free operation with its advanced control system and redundant communication architecture.

Power: 60 W
Thrust Speed Unloaded: 84 mm / sec
Thrust Speed Loaded: 73 mm / sec
Maximum Continuous Force: 523 N
Maximum Force: 3.293 N
Operating Temperature: -40 ° C… .. + 65 ° C

The Landing Gear Linear Actuator is designed and manufactured to meet the performance requirements of modern UAV Flight Control Systems. The BLS-L-040 provides fail-safe and vibration-free operation with its advanced control system and redundant communication architecture.

Power: 40 W
Thrust Speed Unloaded: 22 mm / sec
Thrust Speed Loaded: 18 mm / sec
Maximum Continuous Force: 461 N
Maximum Force: 2.463 N
Operating Temperature: -40 ° C +. + 65 ° C
Weight: 0,707 kg

The BDS-008 Rotary Servo Actuator is designed and manufactured to meet the performance requirements of modern UAV Flight Control Systems. The BDS-008 provides fail-safe and vibration-free operation with its advanced control system and redundant communication architecture.

Power: 8.0 W
Maximum Continuous Torque: 1.3 Nm
Max Torque: 3.5 Nm
Operating Temperature: -40 ° C +. + 65 ° C
Weight: 341 gr

The BDS-208 Dual Redundant Servo Actuator is designed and manufactured to meet the performance requirements of modern UAV Flight Control Systems. With its advanced control system and redundant communication architecture, the BDS-208 provides fail-safe and vibration-free operation.

Power: 80 W
Rated Speed: 132 ° / sec
Maximum Continuous Torque: 1.3 Nm
Max Torque: 3.5 Nm
Operating Temperature: -40 ° C +. + 65 ° C
Weight: 0.670 kg

The Landing Gear Rotary Servo Actuator System is designed and manufactured to meet the performance requirements of modern UAV Flight Control Systems. The BDS-G-040 provides fault-tolerant and vibration-free operation with its advanced control system and redundant communication architecture.

Max Torque: 12 Nm
Maximum Continuous Torque: 10.8 Nm
Operating Temperature: -40 ° C… .. + 65 ° C

The BLS-B-040 Brake System Linear Actuator is designed and manufactured to meet the performance requirements of modern UAV Flight Control Systems. The BLS-B-040 provides fail-safe and vibration-free operation with its advanced control system and redundant communication architecture.

Power: 40 W
Thrust Speed in Unloaded State: 53 mm / sec
Thrust Speed in Loaded State: 43 mm / sec
Maximum Continuous Force: 410 N
Maximum Force: 2,180 N
Operating Temperature: -40 ° C +. + 65 ° C
Weight: 0.864 kg

The Baykar Bomb Rack Unit was developed in accordance with MIL-STD-8591 and MIL-STD-1760E standards for armed tactical class UAVs. Aluminum alloys are mainly used in production. Military standard connectors are used in original control circuit and hub tie connection designs. The hub tie connector for various ammunition can be positioned at two different points. Different types of holding legs can also be integrated for different diameters.

Design Standard: MIL-STD-8591 and MIL-STD-1760E
Hook Class: 100 lb
Dimensions: 106 mm (E) x 208 mm (W) x 103 mm (H)
Weight: ~ 1,000 g
Construction: Aluminum
Operating Temperature Range: -40 ° C to +60 ° C
Bomb Rack Unit

The BDS-W-040 Control Surface Rotary Actuator is designed and manufactured to meet the performance requirements of modern UAV Flight Control Systems. The BDS-W-040 offers fault-tolerant and vibration-free operation with its advanced control system and redundant communication architecture.

Maximum Continuous Torque: 10.8 Nm
Stop Torque: 50.8 Nm
Rated Speed: 136 ° / sec
Max Rotation Angle: ± 120
Operating Temperature: -40 ° C… .. + 65 ° C
Swing when unloaded: <1 º
Weight: 0.730 kg

Bayraktar Digital Communication Link is a data link system that can transmit multiple video and telemetry / telecom data in two ways. It is capable of compressing and transmitting 3 HD and 3 SD video simultaneously with its six h265 video compression engines. In addition to video data, it can receive telemetry and telecom data from various interfaces (RS-232, RS-485, CAN, Ethernet) and transmit bi-directionally with very low latency.

• Low cost and low SWaP
• System components: AMT + GMT + LNA + PA + OYAS
• LOS range up to 200 km
• Ku-band / C-Band operating frequency

The Bayraktar Mini UAV Video Link is an analog video and audio transceiver designed for demanding environments. It is ideal for applications such as law enforcement oversight operations and inspections that require high-precision video and audio transmission in a compact volume.

Real-time Video Surveillance
Law Enforcement Applications
Unmanned Aerial and Land Vehicles
Hidden Wireless Video and Audio Transmission
 

The Bayraktar Digital Image Link is a low cost and low weight image transmission system for Intelligence, Surveillance and Detection (IGK) applications. It features a dual H.264 compression engine that can encode HD and SD videos up to 1080p resolution. In addition to its dual integrated H.264 compression, the decoding of HD-SDI and analog video is also built into the card. As an end-to-end solution, Baykar's Digital Video Link system does not require additional hardware for use

Bayraktar Numerical with RX and PA
LOS range up to 150 km
L, S or C-Band
Dimension: 136.6 mm (E) x 118 mm (W) x 52 mm (H)
Weight: -326 gr
Operating temperature range: -40 ° C to + 65 ° C

The KM-301 is a compact 3-axis magnetometer that can be used as a subsystem to provide orientation output for the navigation system. Its set-reset capability improves system accuracy by eliminating possible strong magnetic disturbance effects and sensor-borne noise.

50 Hz Continuous Output
Hard and Soft Magnetic Calibration Adjustment
Mounting Adjustment Using DCM
Error Detection Output for Sensor and Communication Faults

The GSS Charging Unit is for charging and discharging batteries used by the Bayraktar Aerial Vehicle System.  The batteries are low weight and carry high energy capacity.

Operating Temperature: -40 ºC ..... + 55 ºC
Battery Charge Voltage: 25.2 VDC
Battery Charge Current: 9.3A (max) 
Dimensions: 104mm X 45mm X 66mm
Weight:  160gr.

The Bayraktar digital video link receiver is a low-cost and low-swap video reception system for Intelligence, Surveillance and Reconnaissance (ISR) applications. As a complete end-to-end solution, Baykar’s digital video link receiver requires no additional hardware for deployment.

RF to ethernet based receiver unit
Integrated LNA (0.56dB NF)
Various video formats: 1080p30, 1080p25, 1080i60, 720p60, PAL, NTSC
Size: 119x118x40 mm
Weight: 320 g
Operation temp range: -40 C to +60 C
 

Installed in the Ground Control Station, The Display Command Module enables operators to control and command the key panel, throttle lever unit and joystick.

Operating Temperature: -40 ºC ..... + 55 ºC
Nominal Current: 90 mA
Operating Voltage Level: 24 VDC
Dimensions: 202 mm × 25 mm × 133 mm
Weight: 370 g

The Throttle Lever Unit enables both pilots to moderate commands for the propulsion and braking system and payload operators to command the gimbal camera system.

Modularized fly-by-wire system interface
Ergonomically designed human interface: Easy and effiecient to operate

Operating Temperature: -40 ºC ..... + 55 ºC
Operating Voltage Level: 24 VDC
Nominal Current: 20 mA
Dimensions: 188 mm × 156 mm × 170 mm