National Repository of Grey Literature 3 records found  Search took 0.01 seconds. 
Haptic feedback device design for aircraft control
Dubnický, Lukáš ; Jebáček, Ivo (referee) ; Zikmund, Pavel (advisor)
This master thesis is focused on design of control stick grip and rudder pedals extension. These components are equipped with active elements, which provide pilot with haptic feedback. The purpose of the introduced design is to allow prototype to be built into the aeroplane so that the proposed concept of haptic feedback can be tested onboard. It shall verify used technical solutions as well to allow for their application on following development stages that aim at certification of the proposed haptic feedback system to be used in general aviation aeroplanes. The designed components are the successors of prototypes used for experiments carried on flight simulator. The design process follows the requirements of legislation and outcomes of the previous experiments. This thesis follows the design process from setting of the design requirements to mechanical test of 3D printed prototypes.
Recent progress in pilot-aircraft haptic feedback
Suchnová, Klára ; Horpatzká, Michaela (referee) ; Zikmund, Pavel (advisor)
This bachelor thesis deals with the recent progress in pilot-aircraft haptic feedback. Haptic feedback is intended to help the pilot perform his tasks more easily. Above all, it should focus on relieving the strain on his vision and hearing to increase flight safety. It can be used not only for the actual control of the aircraft but also for other tasks such as navigation. Haptic systems bring a lot of advantages in the actual control of the aircraft, but they also have their disadvantages in certain cases.
Haptic feedback device design for aircraft control
Dubnický, Lukáš ; Jebáček, Ivo (referee) ; Zikmund, Pavel (advisor)
This master thesis is focused on design of control stick grip and rudder pedals extension. These components are equipped with active elements, which provide pilot with haptic feedback. The purpose of the introduced design is to allow prototype to be built into the aeroplane so that the proposed concept of haptic feedback can be tested onboard. It shall verify used technical solutions as well to allow for their application on following development stages that aim at certification of the proposed haptic feedback system to be used in general aviation aeroplanes. The designed components are the successors of prototypes used for experiments carried on flight simulator. The design process follows the requirements of legislation and outcomes of the previous experiments. This thesis follows the design process from setting of the design requirements to mechanical test of 3D printed prototypes.

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