A conceptual design of a general aviation hands-on-throttle and stick (HOTAS) system
Abstract (Summary)
In this project the concept of Hands-on-Throttle and Stick (HOTAS) was applied to a
general aviation (GA) aircraft. HOTAS had seen limited use in GA aircraft, but nothing
that would compare to its use in military or commercial aircraft. The purpose of
incorporating HOTAS was to give the pilot the ability to quickly and efficiently operate
specific functions of the aircraft’s avionics units without having to remove his/her hands
from the stick (or control wheel) or throttle.
This project followed the systems engineering approach to accomplish the conceptual
design of the GA HOTAS system. Two representative GA aircraft were chosen along
with the avionics units to be controlled. In-flight functions of the units were determined
and broken down into their most basic functions. Hardware was identified for each
function, and the best alternative was chosen for each function. A control layout was
achieved and then integrated into the aircraft’s existing controls. The project resulted in a
conceptual GA HOTAS system that could be integrated into existing GA aircraft with
existing avionics.
Throughout the course of this project, the design proceeded with the needs and
abilities of the pilot in mind. The HOTAS system was designed to be operable by pilots
of various sizes and experience levels. The system was meant to be intuitive so that any
pilot with experience in the aircraft’s avionics could operate it; however, training and
experience with the system was also required.
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Bibliographical Information:
Advisor:
School:The University of Tennessee at Chattanooga
School Location:USA - Tennessee
Source Type:Master's Thesis
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