Servo Actuator Units

The Model (BDS-008) Rotary Servo Actautor System is desingned and built to match performance characteristics of modern UAV Flight Control Systems. BDS-008 Provides Failsafe and Jittetless Performance with its Robust Advanced Control System and Redundant Communication Architecture.

Technical Features
Rotary Servo Actuator
Dual Reduntant Communication via CANbus & RS485
Advanced Winding Temperature Estimation Algorithms
Brushless Permanent Magnet DC Motor
End User Software Parameters such as Dead Band-Null Position-Current Limits-Temperature Limits
Precision CNC Machined Aerospace Grade Aluminium Casing
Detailed Diagnostics Data Capability for Testing or Working Purpose
Power 8.0 W
Nominal Speed 93 deg/sec
Nominal Torque 1.5 Nm
Max. Continous Torque 2.4 Nm

The Model (BDS-208) Rotary Servo Actautor System is desingned and built to match performance characteristics of modern UAV Flight Control Systems. BDS-208 Provides Failsafe and Jittetless Performance with its Robust Advanced Control System and Redundant Communication Architecture.

Technical Features
Rotary Servo Actuator
Dual Reduntant Communication via CANbus & RS485
Advanced Winding Temperature Estimation Algorithms
Brushless Permanent Magnet DC Motor
End User Software Parameters such as Dead Band-Null Position-Current Limits-Temperature Limits
Precision CNC Machined Aerospace Grade Aluminium Casing
Detailed Diagnostics Data Capability for Testing or Working Purpose
Power 8.0 W (x2)
Nominal Speed 93 deg/sec
Nominal Torque 1.5 Nm
Max. Continous Torque 2.4 Nm

The Model (BDS-W-040) Rotary Servo Actautor System is desingned and built to match performance characteristics of modern UAV Flight Control Systems. BDS-W-040 Provides Failsafe and Jittetless Performance with its Robust Advanced Control System and Redundant Communication Architecture.

Technical Features
Rotary Servo Actuator
Dual Reduntant Communication via CANbus & RS485
Advanced Winding Temperature Estimation Algorithms
Brushless Permanent Magnet DC Motor
End User Software Parameters such as Dead Band-Null Position-Current Limits-Temperature Limits
Precision CNC Machined Aerospace Grade Aluminium Casing
Detailed Diagnostics Data Capability for Testing or Working Purpose
Maks. Torque 12 Nm
Nominal Speed 95 deg/sec
Stall Torque 40 Nm

The Model (BDS-L-040) Rotary Servo Actautor System is desingned and built to match performance characteristics of modern UAV Flight Control Systems. BDS-L-040 Provides Failsafe and Jittetless Performance with its Robust Advanced Control System and Redundant Communication Architecture.

Technical Features
Linear Servo Actuator
Dual Reduntant Communication via CANbus & RS485
Advanced Winding Temperature Estimation Algorithms
Brushless Permanent Magnet DC Motor
End User Software Parameters such as Dead Band-Null Position-Current Limits-Temperature Limits
Precision CNC Machined Aerospace Grade Aluminium Casing
Detailed Diagnostics Data Capability for Testing or Working Purpose
Power 40 W
Nominal Speed 658.8 N
Nominal Torque 12 mm/sec
Max. Continous Torque 941.2 N

The Model (BLS-B-040) Rotary Servo Actautor System is desingned and built to match performance characteristics of modern UAV Flight Control Systems. BLS-B-040 Provides Failsafe and Jittetless Performance with its Robust Advanced Control System and Redundant Communication Architecture.

Technical Features
Linear Servo Actuator
Dual Reduntant Communication via CANbus & RS485
Advanced Winding Temperature Estimation Algorithms
Brushless Permanent Magnet DC Motor
End User Software Parameters such as Dead Band-Null Position-Current Limits-Temperature Limits
Precision CNC Machined Aerospace Grade Aluminium Casing
Detailed Diagnostics Data Capability for Testing or Working Purpose
Power 40 W
Nominal Speed 584.9 N
Nominal Torque 29.1 mm/sn
Max. Continous Torque 835.5 N

The Model (BLS-060) Rotary Servo Actautor System is desingned and built to match performance characteristics of modern UAV Flight Control Systems. BLS-060 Provides Failsafe and Jittetless Performance with its Robust Advanced Control System and Redundant Communication Architecture.

Technical Features
Linear Servo Actuator
Dual Reduntant Communication via CANbus & RS485
Advanced Winding Temperature Estimation Algorithms
Brushless Permanent Magnet DC Motor
End User Software Parameters such as Dead Band-Null Position-Current Limits-Temperature Limits
Precision CNC Machined Aerospace Grade Aluminium Casing
Detailed Diagnostics Data Capability for Testing or Working Purpose
Power 60 W
Nominal Speed 180 N
Nominal Torque 180 mm/sec
Max. Continous Torque 230 N