Determining design guidelines for a haptic admittance display in aircraft control

Master Thesis (2021)
Author(s)

S. Kistemaker (TU Delft - Aerospace Engineering)

Contributor(s)

M. M.(René) van Paassen – Mentor (TU Delft - Control & Simulation)

Max Mulder – Graduation committee member (TU Delft - Control & Simulation)

A Sharpanskykh – Graduation committee member (TU Delft - Air Transport & Operations)

Faculty
Aerospace Engineering
Copyright
© 2021 Sander Kistemaker
More Info
expand_more
Publication Year
2021
Language
English
Copyright
© 2021 Sander Kistemaker
Graduation Date
21-12-2021
Awarding Institution
Delft University of Technology
Programme
Aerospace Engineering
Faculty
Aerospace Engineering
Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Abstract

The haptic feedback signal in haptic interfaces is usually in the form of a force on the control device. In contrast, the “active side stick”, investigated in the 80s and 90s, uses an admittance display, whereby the position of the device is linked to the feedback signal, and force applied on the device is used as the control signal. These devices are usually tuned in a serendipitous manner. To better understand the potential and tuning rules for these devices, tuning is investigated with a model-based approach and verified in pilot-in-the loop experiments using various aircraft dynamics. It was found that certain gain settings offered considerable benefits in terms of tracking performance as well as the control effort exerted by the pilot, while taking into account the system's stability margins. Based on these findings, a comprehensive tuning procedure is proposed for control systems involving an active manipulator.

Files

MScThesis_SanderKistemaker.pdf
(pdf | 14.5 Mb)
- Embargo expired in 21-12-2023
License info not available