Detail výsledku
Autotrim Unit
Dittrich Petr, Ing., Ph.D., FIT (FIT), UPGM (FIT)
Koloničný Alois, Ing., UPGM (FIT)
The autotrim unit alleviates forces in the mechanical flight control system. The unit itself uses the information about the value and the orientation of the control force in the mechanical installation of the primary flight control system and commands the trim actuator, which in turn operates a trim tab at the control surface's trailing edge. The deflections of the trimtab assists in minimizing the loading and the energy requirements needed to hold the primary control surface at a specified deflection.
Avionics, Flight Control, Embedded System, Modular Architecture, CAN aerospace, Trim
Laboratoř Aeroworks (místnost L209), Fakulta informačních technologií VUT v Brně, Božetěchova 2, 612 66 Brno http://www.fit.vutbr.cz/research/prod/index.php.cz?id=299
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