Products
Unmanned Platforms
FSA100-0000-00
FSA100-0000-00 rotary servo actuators are flight-proven with 50,000+ flight hours. These actuators are currently used as air intake actuators on unmanned platforms.
FSA100 series actuators produce 1.1Nm nominal torque at 180°/s nominal speed.
- Auxiliary control servo actuator
- Flight-proven, 50,000+ flight hours
- In-flight health monitoring
- High power-to-weight ratio
FSA101-0000-00
FSA101-0000-00 rotary servo actuator is used to position the primary and secondary flight control surfaces on unmanned platforms. These actuators are flight proven with 120,000+ flight hours.
- Primary & secondary flight control surface servo actuator
- Flight-proven, 120,000+ flight hours
- In-flight health monitoring
- High power-to-weight ratio
- Compatible with MIL- STD-461E and MIL-STD-810G
FSA101-0000-01
FSA101-0000-01 rotary servo actuator is used to position the primary and secondary flight control surfaces on unmanned platforms. Being a variant of FSA101 series, FSA101-0000-01 actuators differ with the integrated electromagnetic brake. These actuators are flight proven with 25,000+ flight hours.
- Primary & secondary flight control surface servo actuator
- Flight-proven, 25,000+ flight hours
- In-flight health monitoring
- High power-to-weight ratio
- Compatible with MIL- STD-461E and MIL-STD-810G
FSA102-0000-00
FSA102 rotary servo actuators are used to position the primary and secondary flight control surfaces on unmanned platforms. These actuators are currently in use in various unmanned platforms, with accumulated flight hours over 60,000.
- Primary & secondary flight control surface servo actuator
- Flight-proven, 60,000+ flight hours
- In-flight health monitoring
- Lightweight structure (Actuator + Controller)
- Compatible with MIL- STD-461E and MIL-STD-810G
FSA201-0000-00
FSA201-0000-00 series are linear servo actuators designed for unmanned platforms, delivering 200N rated force. These actuators are electronically and mechanically redundant. FSA201 series actuators are used for primary flight control surfaces, with accumulated flight hours of 250,000+.
- Redundant primary flight control
- Flight-proven, 250,000+ flight hours
- In-flight health monitoring
- Lightweight Structure (Actuator + Controller)
Manned Fixed-Wing Platforms
GSE101-0000-06
Developed for a civil aviation platform and integrated into wing structure to control spoiler flight control surface. Special feedback mechanism and sensor unit provides absolute positioning. Civil aviation certification process completed.
- Rotary absolute positioning sensor
- Anti-rotation system
- Retractable under 300N
ASD101-0000-02
ASD101-0000-02 is a controller unit which controls for 2 GSE101-0000-06 units simultaneously.
Filter, controller and driver card is designed to meet DO160 (Environmental Conditions) and DO254 (Hardware Specifications). The product is compliant to civil aviation standards. It can be customized for various types of servo actuators.
- High accuracy control
- Integrated to mechanical flight controls
- High performance output
HRP101-0000-00
Developed for use in the jet trainer’s fly-by-wire flight control system, the Rudder Pedal equipment converts pilot commands into input signals to the rudder function, brake function and nose gear steering function. This equipment also has mechanisms that provide artificial feeling to the pilot while performing the rudder, braking and steering functions.
An electromechanical actuator that adjusts the pedal distance to ensure comfortable use by pilots of varying heights is also part of the Rudder Pedal equipment.
An electromechanical actuator that adjusts the pedal distance to ensure comfortable use by pilots of varying heights is also part of the Rudder Pedal equipment.
- Redundant architecture tailored with aircraft systems
- Customized artificial feeling
- Lightweight structure
- Customized for HMI Considerations
Manned Rotorcraft Platforms
TS100
TS1000 is a rotary type electromechanical trim actuator designed for use on a civil utility rotorcraft.
It is integrated into the helicopter rotor flight control system and transfers the commands from the autopilot computer to the mechanical flight control system as physical movement. Then mechanical flight control system provides control input to the servo hydraulic actuators that actuate the primary controls of the helicopter. When the autopilot mode is disabled, trim actuators provide the pilot an artificial feeling under normal flight scenarios, thus providing a more controlled and comfortable flight. Additionally, the trim actuator is used for the neutral point of the controls for a trimmed flight.
- Unique design for manned platforms
- High precision control at the output shaft
- Lightweight structure
- Redundant Architecture
- Customized Artificial Feeling
- Anti Backlash system at the output shaft
EMB101-0000-00
Developed by ANDAR for a CS27 certified helicopter program to integrate into primary flight control surfaces, EMB101 electromagnetic brake has a highly specialized and customized structure, designed to meet customer requirements. It provides high holding torque with its specially designed structure and special material.
The electromagnetic brake is integrated into the trimming system, allowing the pilot to manually adjust the neutral point of the controller by releasing the brake and holding the newly trimmed neutral point. It provides comfortable control to the pilot depending on the changes in flight conditions.
The electromagnetic brake is integrated into the trimming system, allowing the pilot to manually adjust the neutral point of the controller by releasing the brake and holding the newly trimmed neutral point. It provides comfortable control to the pilot depending on the changes in flight conditions.
- High holding torque
- Lightweight structure
- Minimal backlash
RBS101-0000-00
Rotor Brake System consists of an electromechanical brake with floating caliper and its control box.
The rotor brake functions at a point connecting the main rotor and tail rotor in the helicopter and has the capacity to stop both of them. The main purpose of the system is to stop the rotor after the helicopter landing and enable comfortable evacuation.
The rotor brake functions at a point connecting the main rotor and tail rotor in the helicopter and has the capacity to stop both of them. The main purpose of the system is to stop the rotor after the helicopter landing and enable comfortable evacuation.
- Unique integrated design of brake and controller
- Robust system for harsh environment
- Lightweight structure with carbon disc and pad
- Safety critical equipment
Urban Air Mobility Vehicles
FSA100-0000-00
FSA100-0000-00 rotary servo actuators are flight-proven with 50,000+ flight hours. These actuators are currently used as air intake actuators on unmanned platforms.
FSA100 series actuators produce 1.1Nm nominal torque at 180°/s nominal speed.
- Auxiliary control servo actuator
- Flight-proven, 50,000+ flight hours
- In-flight health monitoring
- High power-to-weight ratio
FSA101-0000-00
FSA101-0000-00 rotary servo actuator is used to position the primary and secondary flight control surfaces on unmanned platforms. These actuators are flight proven with 120,000+ flight hours.
- Primary & secondary flight control surface servo actuator
- Flight-proven, 120,000+ flight hours
- In-flight health monitoring
- High power-to-weight ratio
- Compatible with MIL- STD-461E and MIL-STD-810G
FSA101-0000-01
FSA101-0000-01 rotary servo actuator is used to position the primary and secondary flight control surfaces on unmanned platforms. Being a variant of FSA101 series, FSA101-0000-01 actuators differ with the integrated electromagnetic brake. These actuators are flight proven with 25,000+ flight hours.
- Primary & secondary flight control surface servo actuator
- Flight-proven, 25,000+ flight hours
- In-flight health monitoring
- Lightweight structure (Actuator + Controller)
- Compatible with MIL- STD-461E and MIL-STD-810G
FSA102-0000-00
FSA102 rotary servo actuators are used to position the primary and secondary flight control surfaces on unmanned platforms. These actuators are currently in use in various unmanned platforms, with accumulated flight hours over 60,000.
- Primary & secondary flight control surface servo actuator
- Flight-proven, 60,000+ flight hours
- In-flight health monitoring
- Lightweight structure (Actuator + Controller)
- Compatible with MIL- STD-461E and MIL-STD-810G
FSA201-0000-00
FSA201-0000-00 series are linear servo actuators designed for unmanned platforms, delivering 200N rated force. These actuators are electronically and mechanically redundant. FSA201 series actuators are used for primary flight control surfaces, with accumulated flight hours of 250,000+.
- Redundant primary flight control
- Flight-proven, 250,000+ flight hours
- In-flight health monitoring
- Lightweight structure (Actuator + Controller)
Space & Guidance Platforms
GSE101-0000-00
GSE101-0000-00 is designed and developed for use in guidance systems. Indigenous design includes a high power slotless BLDC motor along with gearbox and encoder.
- Incremental rotary encoder
- Field-proven
- Configurations for different stroke, load & speed
- Optional absolute position feedback
- Optional Holding Brake
GSE101-0000-03
This actuator is a variant of GSE101-0000-00 where mechanical joint geometry and operating range are customized for the application.
- Incremental rotary encoder
- Field proven
GSE101-0000-05
A variant of GSE101-000-00 where mechanical joint geometry and operating range are customized for the application. Includes a linear absolute positioning sensor and anti-rotation system.
Linear absolute positioning sensor
Anti-rotation system
Linear absolute positioning sensor
Anti-rotation system
GSE101-0000-09
Includes the highest dynamic and static load limits among GSE101 product family along with linear absolute positioning sensor and anti rotation system.
Linear Absolute Positioning Sensor
High Static Load Limit
Anti-rotation system
Linear Absolute Positioning Sensor
High Static Load Limit
Anti-rotation system
GSE102-0000-00
This solution is designed specifically for circumstances with volume and interface limitations. Parallel configuration of the motor and output drive with an intention to reduce products total length.
Linear Absolute Positioning Sensor
Anti-rotation System
Linear Absolute Positioning Sensor
Anti-rotation System
GSE103-0000-00
This product includes a 900W output power slotless BLDC motor, planetary gear box, electromechanical power-off brake, and incremental rotary encoder.
Incremental rotary encoder
Power-off brake
High power density planetary gearbox
High stroke capacity
Incremental rotary encoder
Power-off brake
High power density planetary gearbox
High stroke capacity