Flight Control Systems

Flight Control Computer – designed, developed and manufactured by Baykar capabilities- is a leader avionics unit in its class worldwide. It is the main mission computer that performs the flight critical operations on the aerial platform.

General Features
Autonomous Cruise
Autonomous Taxi and Parking
Sensor Fusion Aided Precise Take off and Landing
Advanced Fuel Level Control and Compensation System
Redundant Control System Architecture
Modern Non-Lineer Control Techniques
Modern Stochastic Filters
Redundant Communication Architecture
Technical Features
Operating temperature: -40°C to +55°C
Environmental compatibility (MIL-STD-810F)
Electromagnetic compatibility (MIL-STD-461F)
MIL-DTL-38999 series connector
Triple Redundant System Architecture
Functioning With Full Performance Even in Case of Critical Failure
Redundant Communication Interfaces With All Other Avionics Units
Conductional Cooling Technique
Modularity With Replaceable Small Form Factor Modules
Ease of Operation And Maintenance

Mission Control Computer – designed, developed and manufactured by Baykar capabilities- is the avionics unit that performs the mission critical operations on the aerial platform.

General Features
Operating temperature: -40°C to +55°C
Environmental compatibility (MIL-STD-810F)
Electromagnetic compatibility (MIL-STD-461F)
MIL-DTL-38999 series connector
Redundant Communication Interfaces With All Other Avionics Units
Conductional Cooling Technique
Modularity With Replaceable Small Form Factor Modules
Ease of Operation And Maintenance

Mini Flight Control Computer – designed, developed and manufactured by Baykar capabilities- is used as the main avionics control unit in Bayraktar Mini UAS. It receives the flight data provided by the sensor units, runs the control algorithms and controls the actuators and payload systems on the aerial platform..

General Features
More Than 100.000 Hours Test/Operational Experience
Low Power Consumption
High Thermal Performance
Developable System Capabilities(CPU Performance, Input/Output Interfaces etc.)
Hardware And Software Configurable for Several Applications
Low Size and Weight

Precise Inertial Measurement Unit is used for attitude determination in aircrafts. It is used as the primary sensor in sensor fusion and stochastic filtering applications.

General Features
Operating temperature: -40°C to +55°C
Environmental compatibility (MIL-STD-810F)
Electromagnetic compatibility (MIL-STD-461F)
MIL-DTL-38999 series connector
Angular rate measurement range: ± 800 °/s
Acceleration measurement range: ± 40 g
High measurement range
Low angular rate noise
Precise attitude estimation
Redundant communication with diverse interfaces
Configurable communication protocol for different hardware and software applications

Baykar Inertial Measurement Unit(BIMU) is used for attitude determination of the aerial platform. BIMU- designed, developed and manufactured by Baykar capabilities- is used as the primary sensor in sensor fusion and stochastic filtering applications.

General Features
Operating temperature: -40°C to +55°C
Environmental compatibility (MIL-STD-810F)
Electromagnetic compatibility (MIL-STD-461F)
MIL-DTL-38999 series connector
High Sensivity Sensors
Self Eliminating Any Temperature and Aging Effects
High Immunity to Shock and Vibration
Redundant Communitacion With Diverse Interfaces
Configurable Communication Protocol for Different Hardware and Software Applications
In-case Heating and Automatic Temperature Control

Mini Inertial Measurement Unit(MIMU) is used for attitude determination of the aerial platform. MIMU- designed, developed and manufactured by Baykar capabilities- is used as the primary sensor in sensor fusion and stochastic filtering applications.

General Features
Operating temperature: -40°C to +55°C
Environmental compatibility (MIL-STD-810F)
Electromagnetic compatibility (MIL-STD-461F)
High Sensivity Sensors
Self Eliminating Any Temperature and Aging Effects
High Immunity to Shock and Vibration
Configurable Communication Protocol for Different Hardware and Software Applications
In-case Heating and Automatic Temperature Control

Pitot-Static Probes are used for delivering total and static pressure information to desired units which determines velocity and altitude in aircrafts.

General Features
Anti-ice Heating System
High Sensivity in All Wecther Conditions
High Moduler Structure (System)
Special Designed Water Drainage System

Pitot-Static-Alpha-Beta Unit consists of pressure sensors for measuring the altitude and airspeed of the aircraft and also an interface to integrate sensors that measure angle-of-attack and sideslip angles.

General Features
Operating temperature: -40°C to +55°C
Environmental compatibility (MIL-STD-810F)
Electromagnetic compatibility (MIL-STD-461F)
MIL-DTL-38999 series connector
Pressure sensors that have internal compensation and calibration
High resolution Alpha and Beta sensors that are specially designed for the requirements
Redundant communication with diverse interfaces
Configurable communication protocol for different hardware and software applications
In-case heating and automatic temperature control

Pitot – Magnetometer Unit consists of pressure sensors for measuring the altitude and airspeed of the aircraft and the precision magnetic sensors for receiving the compass information.

General Features
Operating temperature: -40°C to +55°C
Environmental compatibility (MIL-STD-810F)
Electromagnetic compatibility (MIL-STD-461F)
MIL-DTL-38999 series connector
Pressure sensors that have internal compensation and calibration
High resolution magnetic sensors with high accuracy
Redundant communication with diverse interfaces
Configurable communication protocol for different hardware and software applications
In-case heating and automatic temperature control

Baykar Global Navigation Satellite System (GNSS) receiver offers precise position, velocity and attitude measurements by using GPS, GLONASS, SBAS, Galileo, BeiDou and QZSS satellites with up to 50 Hz data output rate. Sub-centimeter accurate position solutions are possible with the inherent Real Time Kinematic (RTK) system.

General Features
Sub-centimeter position accuracy
Redundant communication with diverse interfaces
Configurable communication protocol
Ruggedized case with low size and weight
Position Measurements
GPS L1 C/A, L2E, L2C, L5
GLONASS L1 C/A, L1 P, L2 C/A, L3
SBAS Simultaneous L1 C/A, L5
GALILEO L1 BOC, E5A, E5B, E5AltBOC
BeiDou B1, B2
QZSS L1 C/A, L1 SAIF, L2C, L5
Vector Measurements
GPS Simultaneous L1 C/A, L2E, L2C
GLONASS Simultaneous L1 C/A, L2 C/A, L2P
BeiDou B1
Accuracy
Differential Code 0.25 m + 1 ppm Horizontal, 0.50 m + 1 ppm Vertical
SBAS < 5 m (3DRMS)
RTK ( <30 km) ± 8 mm + 1 ppm Horizontal,  ± 15 mm + 1 ppm Vertical (RMS)
Attitude (2 m baseline) < 0.09°
Advanced Features
Typical Start Time < 10 seconds
Operating Temperature -40°C to +75°C
Communication 1xCAN, 4xRS232, 1 LAN