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Presented work discusses a proposal of an environmentally friendly flight control system for Light Aircraft or Unmanned Air Vehicle (UAV). The noise and emissions reducing flight control system is based on Total X Control System (TXCS) and assumes the reduction of the total energy dissipation. A general description of the flight control system, control laws, as well as results of preliminary tests...
This paper presents the results of Pilot Assisting Module research performed on two light aircraft flight simulators developed in parallel at Brno University of Technology, Czech Republic, and Rzeszow University of Technology, Poland. The first simulator was designed as an open platform for the verification and validation of the advanced pilot/aircraft interface systems and inherited its appearance...
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