Purpose of the development: On the basis of the proposed method is designed to optimize the robust flight control system and automatic piloting system for small unmanned aerial vehicles (UAVs), whose altitude of 2000 m, the range of 500-600 km and a speed of 250-300 km / h.

Recommended application field: Aircraft.

Advantages over analogues: Systems are different from other simple, highly accurate stabilization of flight parameters in the volatile atmosphere and robustness relative to change the subject.

The development stage readiness: Tested experimental exploitation order

Description of the development:
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Proposed a set of algorithms and programs of the software for flight management systems and flight control of small UAV made ??in MATLAB and SIMULINK allowing for the class of UAV flight tasks and possibilities of using flight data sensors (GPS and air data system). Systems are implemented and tested in flight.

corresponds technical description
Ready for implementation

Possibility of transfer abroad:
Licence's sale
Technological document's sale
Combinated reduction to industrial level

Photo

Country Ukraine

For additional information turn to:
E-mail: gal@uintei.kiev.ua