Defining the technical conceptual product corresponds to customer's request.

Performing system engineering of products and onboard control system integrally.

Selecting the product list based on a wide range device set: computing machine, navigation processing devices, measurement devices, actuators, communication systems

The design process is followed by engineering mechanical structures analysis, including composite materials analysis. According to the results, perform the optimization taking into account technological and economic project limits.

Performing CFD aerodynamic calculation to obtain the product aerodynamic characteristics for control synthesis and validation of design characteristics.

Executing the flight control systems development and final adjustment of various aircraft types. Relying on unique hardware, software and practical experience: 

• mathematical motion model development
• automatic development and flight control synthesis
• navigation and trajectory control level integration
• behavior logic control rules and equipment synthesis
• simulation system in the complex (hardware-in-loop)
• flight tests for testing and verification the mathematical model by experimental dynamic motion model identification 

Performing a full set of UAVs flight tests to confirm the specifications stated.

• Integrating the payload with required components. Relying on existing experience in the field of electro-optical systems in the optical and infrared ranges.
• Performing hardware and software interfacing with onboard payloads to control complexes of specialized types

Integration of UAVs wireless communication systems:

• design of systems based on existing background in software-defined radio systems
• development of communication devices according to customer requirements
• development and production of specialized antennas
• integration with IP networks
• integration of software and hardware solutions for creation of ad-hoc mesh-networks
• providing of communication system flight tests involving manned or unmanned aviation

Testing of envirinmental resistance:

• sinusoidal vibrations
• broadband vibration
• shock testing
• thermal tests ranging from -70°C to +150°C
• humidity in the range of 0-100%
• qualification of products for compliance with the qualification criteria

Designing a series of powerplants adapted to parts of product:

• fuel system based on electronic injection
• detachable equipment
• exhaust system
• special composition solutions

Pilot metal-working manufacturing with CNC machine centers providing:

Pilot composite manufacturing based on the following technologies:

• manual lamination
• vacuum infusion
• prepreg sintering
• resin transfer moulding