Proceedings of the 3rd Annual International Conference on Mechanics and Mechanical Engineering (MME 2016)

Adaptive Observer for Multi-Effectors Aircraft with Control Surface Damage

Authors
Shuang Zhang
Corresponding Author
Shuang Zhang
Available Online December 2016.
DOI
https://doi.org/10.2991/mme-16.2017.103How to use a DOI?
Keywords
Multi-effectors aircraft, Control surface damage, Fault diagnosis. Adaptive compensation observer.
Abstract
An adaptive compensation observer is presented for fast diagnose of multi-effectors aircraft in the presence of control surfaces fault, which directly estimates the deflection angles of control surfaces. An augmented observer is designed for the estimation of system input, and an adaptive compensation is introduced to improve the dynamic tracking performance of observer. Simulation results suggest that, for different cases of actuator faults, the proposed observer methods can achieve fault alarm within 20 milliseconds and determine the fault location in 0.22 seconds.
Open Access
This is an open access article distributed under the CC BY-NC license.

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Proceedings
3rd Annual International Conference on Mechanics and Mechanical Engineering (MME 2016)
Part of series
Advances in Engineering Research
Publication Date
December 2016
ISBN
978-94-6252-303-6
ISSN
2352-5401
DOI
https://doi.org/10.2991/mme-16.2017.103How to use a DOI?
Open Access
This is an open access article distributed under the CC BY-NC license.

Cite this article

TY  - CONF
AU  - Shuang Zhang
PY  - 2016/12
DA  - 2016/12
TI  - Adaptive Observer for Multi-Effectors Aircraft with Control Surface Damage
BT  - 3rd Annual International Conference on Mechanics and Mechanical Engineering (MME 2016)
PB  - Atlantis Press
SN  - 2352-5401
UR  - https://doi.org/10.2991/mme-16.2017.103
DO  - https://doi.org/10.2991/mme-16.2017.103
ID  - Zhang2016/12
ER  -