This paper discusses the design and simulation of the Total-X flight control concept. Total-X has been implemented into the flight control logic of a light aircraft's flight control system. This implementation has been subjected to numerous simulations using rapid prototyping and real-time simulation environments. The advantage of the Total-X system proved to be in excellent performance and moderate complexity of the resulting controller structure compared to classical control law design.

@INPROCEEDINGS{
   author = {Peter Chudý and Pawel Rzucidlo},
   title = {Simulations of Total-X based flight control system for light
	aircraft},
   pages = {1--8},
   booktitle = {Conference of Avionics},
   year = {2010},
   location = {Bezmiechowa, PL},
   publisher = {Rzesow University of Technology},
   ISBN = {978-83-7199-623-8},
   language = {english},
   url = {http://www.fit.vutbr.cz/research/view_pub.php?id=9264}
}