Abstract

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 performed on a LSA flight simulator are presented in the following parts of this paper.

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