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Applications

Different systems. Measurable engineering decisions.

From flight-control development and avionics validation to production quality control and research, test infrastructure should be designed around the system under evaluation. INFINITE-HIL brings real hardware together with controlled motion, measurement and simulation to provide configurable engineering solutions across applications.

Vehicle or product geometry, target physical behaviour, instrumentation, software interfaces and budget are assessed together. Alongside X1’s three-axis architecture, custom test machines and aerospace test and simulation platforms can be designed for project-specific needs in other industries.

Multirotor UAV seen from above

INFINITE-HIL · Drone attitude control test rig

Multirotor UAVs

Develop attitude control on the physical vehicle. Examine control response, sensor fusion and mechanical-integration effects on quadcopters and other multirotor platforms using controlled motion profiles. Vehicle-specific fixtures and instrumentation support comparison of settings or product revisions within the same scenario.

  • PID and control-parameter comparison
  • IMU/magnetometer evaluation
  • Revision comparison and production test profiles
Fixed-wing UAV in flight

INFINITE-HIL · Fixed-wing autopilot HIL testing

Fixed-wing UAVs

Evaluate fixed-wing avionics, autopilot and attitude control in the laboratory. Flight controllers, orientation estimation and suitable control interfaces can be examined alongside physical attitude motion. Fixture and motion envelope are designed around wing geometry, centre of mass and test objectives; this scope is distinct from aerodynamic performance testing.

  • Attitude estimation
  • Control and interface integration
  • Sensor comparison at defined orientations
VTOL UAV with lift rotors in flight

INFINITE-HIL · VTOL flight control HIL testing

VTOL and hybrid aircraft

Examine VTOL and hybrid flight-control logic across multiple flight modes within a shared HIL test approach. Algorithms, sensor responses and transition logic for vertical and forward-flight modes can be evaluated through scenarios configured with suitable models and hardware interfaces. Scope is defined around the vehicle architecture and behaviour to be validated.

  • Mode-transition logic
  • Combined attitude profiles
  • Model and control-hardware integration
Close-up of an electronic circuit board

INFINITE-HIL · Flight controller test bench

Flight-controller and avionics manufacturers

Measure the interaction between algorithms and hardware. Evaluate board, sensor and software updates using physical motion, angular reference and coordinated data. Repeatable profiles provide a shared basis for revision comparison and sensor-integration studies.

  • Regression testing
  • Sensor orientation and calibration
  • Data interfaces and control feedback
Unmanned aerial platform during a field test

INFINITE-HIL · Custom UAV test infrastructure

Defence technologies and local test infrastructure

Configurable infrastructure for institutional validation workflows. Bring control, instrumentation and test software into one engineering scope for autonomous platforms, avionics and orientation-sensitive sensors. Mechanical design and integration are adapted to institutional interfaces and test requirements.

  • Integration with in-house control infrastructure
  • Repeatable laboratory scenarios
  • Project-specific measurement and data workflows
Researcher working at a laboratory test setup

INFINITE-HIL · 3-DOF platform for control research

Academia and research

Test models through physical experiments. Combine real hardware, measurement and simulation in control theory, sensor fusion and system-identification studies. The modular approach allows fixture, sensing and software options to be selected for research scope and laboratory budget.

  • Control experiments
  • Model-to-measurement comparison
  • Adaptable setups for student and research projects
Small satellite in orbit above the Earth

INFINITE-HIL · CubeSat ADCS research setup

Small-satellite ADCS research

An adaptable approach to satellite attitude-determination and control research. Three-axis motion and angular measurement can be adapted to ADCS laboratory work, such as CubeSat attitude control testing and hardware-in-the-loop experiments, through suitable mechanical and sensor configurations. Experiments involving reaction wheels, magnetic environments or mission conditions require dedicated definition; space qualification is not assumed for a standard X1.

  • Attitude estimation
  • Laboratory control research
  • Project-specific mechanical and data integration
  • HAVELSAN JET CUBEIncubation programme
  • Teknopark İstanbulCube Incubation
  • ArduPilot · PixhawkLaboratory testing on X1

Your application

Let’s design the test system your application requires.

For needs beyond a standard configuration, we can assess mechanical design, custom machine manufacturing, instrumentation and software integration within one project scope.

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