Navigation and control based on integral-uncertainty observer for unmanned jet aircraft

A nonlinear integral-uncertainty observer is presented, which can estimate the integral of measurement output signal and the uncertainty in system, synchronously. In order to be satisfied with the existing hardware computational environments and to select the parameters more easily, a simplified lin...

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Main Authors: Wang, Xinhua, Cai, Lilong
Format: Article
Published: Institute of Electrical and Electronics Engineers 2017
Subjects:
Online Access:https://eprints.nottingham.ac.uk/41811/
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author Wang, Xinhua
Cai, Lilong
author_facet Wang, Xinhua
Cai, Lilong
author_sort Wang, Xinhua
building Nottingham Research Data Repository
collection Online Access
description A nonlinear integral-uncertainty observer is presented, which can estimate the integral of measurement output signal and the uncertainty in system, synchronously. In order to be satisfied with the existing hardware computational environments and to select the parameters more easily, a simplified linear version of the nonlinear integral-uncertainty observer is also developed. The effectiveness of the proposed observers are verified through the numerical simulations and experiments: i) through the integral-uncertainty observers, the attitude angle and the uncertainties in attitude dynamics are estimated synchronously from the measurements of angular velocity, and the estimate results by the two observers are compared; ii) a control law is designed based on the observers to drive the jet aircraft to track a reference trajectory.
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spelling nottingham-418112020-05-04T18:35:03Z https://eprints.nottingham.ac.uk/41811/ Navigation and control based on integral-uncertainty observer for unmanned jet aircraft Wang, Xinhua Cai, Lilong A nonlinear integral-uncertainty observer is presented, which can estimate the integral of measurement output signal and the uncertainty in system, synchronously. In order to be satisfied with the existing hardware computational environments and to select the parameters more easily, a simplified linear version of the nonlinear integral-uncertainty observer is also developed. The effectiveness of the proposed observers are verified through the numerical simulations and experiments: i) through the integral-uncertainty observers, the attitude angle and the uncertainties in attitude dynamics are estimated synchronously from the measurements of angular velocity, and the estimate results by the two observers are compared; ii) a control law is designed based on the observers to drive the jet aircraft to track a reference trajectory. Institute of Electrical and Electronics Engineers 2017-02-13 Article PeerReviewed Wang, Xinhua and Cai, Lilong (2017) Navigation and control based on integral-uncertainty observer for unmanned jet aircraft. IEEE Transactions on Aerospace and Electronic Systems . pp. 1-20. ISSN 0018-9251 Integral-uncertainty observer jet aircraft attitude angle uncertainty synchronous estimate http://ieeexplore.ieee.org/document/7851055/ doi:10.1109/TAES.2017.2668078 doi:10.1109/TAES.2017.2668078
spellingShingle Integral-uncertainty observer
jet aircraft
attitude angle
uncertainty
synchronous estimate
Wang, Xinhua
Cai, Lilong
Navigation and control based on integral-uncertainty observer for unmanned jet aircraft
title Navigation and control based on integral-uncertainty observer for unmanned jet aircraft
title_full Navigation and control based on integral-uncertainty observer for unmanned jet aircraft
title_fullStr Navigation and control based on integral-uncertainty observer for unmanned jet aircraft
title_full_unstemmed Navigation and control based on integral-uncertainty observer for unmanned jet aircraft
title_short Navigation and control based on integral-uncertainty observer for unmanned jet aircraft
title_sort navigation and control based on integral-uncertainty observer for unmanned jet aircraft
topic Integral-uncertainty observer
jet aircraft
attitude angle
uncertainty
synchronous estimate
url https://eprints.nottingham.ac.uk/41811/
https://eprints.nottingham.ac.uk/41811/
https://eprints.nottingham.ac.uk/41811/