Aircraft navigation based on differentiation–integration observer
In this paper, a generalized differentiation–integration observer is presented based on sensors selection. The proposed differentiation–integration observer can estimate the multiple integrals and high-order derivatives of a signal, synchronously. The parameters selection rules are presented for the...
| Main Authors: | , |
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| Format: | Article |
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Elsevier Masson
2017
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| Online Access: | https://eprints.nottingham.ac.uk/43395/ |
| _version_ | 1848796678220414976 |
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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 | In this paper, a generalized differentiation–integration observer is presented based on sensors selection. The proposed differentiation–integration observer can estimate the multiple integrals and high-order derivatives of a signal, synchronously. The parameters selection rules are presented for the differentiation–integration observer. The theoretical results are confirmed by the frequency–domain analysis. The effectiveness of the proposed observer is verified through the numerical simulations on a quadrotor aircraft: i) through the differentiation–integration observer, the attitude angle and the uncertainties in attitude dynamics are estimated synchronously from the measurements of angular velocity; ii) a control law is designed based on the observers to drive the aircraft to track a reference trajectory. |
| first_indexed | 2025-11-14T19:51:48Z |
| format | Article |
| id | nottingham-43395 |
| institution | University of Nottingham Malaysia Campus |
| institution_category | Local University |
| last_indexed | 2025-11-14T19:51:48Z |
| publishDate | 2017 |
| publisher | Elsevier Masson |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | nottingham-433952020-05-04T19:10:10Z https://eprints.nottingham.ac.uk/43395/ Aircraft navigation based on differentiation–integration observer Wang, Xinhua Cai, Lilong In this paper, a generalized differentiation–integration observer is presented based on sensors selection. The proposed differentiation–integration observer can estimate the multiple integrals and high-order derivatives of a signal, synchronously. The parameters selection rules are presented for the differentiation–integration observer. The theoretical results are confirmed by the frequency–domain analysis. The effectiveness of the proposed observer is verified through the numerical simulations on a quadrotor aircraft: i) through the differentiation–integration observer, the attitude angle and the uncertainties in attitude dynamics are estimated synchronously from the measurements of angular velocity; ii) a control law is designed based on the observers to drive the aircraft to track a reference trajectory. Elsevier Masson 2017-09-30 Article PeerReviewed Wang, Xinhua and Cai, Lilong (2017) Aircraft navigation based on differentiation–integration observer. Aerospace Science and Technology, 68 . pp. 109-122. ISSN 1270-9638 Differentiation–integration observer Multiple integrals Derivatives Quadrotor aircraft http://www.sciencedirect.com/science/article/pii/S127096381730192X doi:10.1016/j.ast.2017.05.007 doi:10.1016/j.ast.2017.05.007 |
| spellingShingle | Differentiation–integration observer Multiple integrals Derivatives Quadrotor aircraft Wang, Xinhua Cai, Lilong Aircraft navigation based on differentiation–integration observer |
| title | Aircraft navigation based on differentiation–integration observer |
| title_full | Aircraft navigation based on differentiation–integration observer |
| title_fullStr | Aircraft navigation based on differentiation–integration observer |
| title_full_unstemmed | Aircraft navigation based on differentiation–integration observer |
| title_short | Aircraft navigation based on differentiation–integration observer |
| title_sort | aircraft navigation based on differentiation–integration observer |
| topic | Differentiation–integration observer Multiple integrals Derivatives Quadrotor aircraft |
| url | https://eprints.nottingham.ac.uk/43395/ https://eprints.nottingham.ac.uk/43395/ https://eprints.nottingham.ac.uk/43395/ |