Attitude and Altitude Control of Unmanned Aerial-Underwater Vehicle Based on Incremental Nonlinear Dynamic Inversion
A vehicle able to navigate both in the air and underwater is referred to an unmanned aerial-underwater vehicle (UAUV). Aiming at the attitude and altitude control of UAUVs, an incremental dynamic inverse control (INDI) method with second-order low-pass filters is proposed. Based on the underwater mo...
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doaj-b5393204fed44150bd5ef966e9fbc93d2021-03-30T04:07:25ZengIEEEIEEE Access2169-35362020-01-01815612915613810.1109/ACCESS.2020.30158579164924Attitude and Altitude Control of Unmanned Aerial-Underwater Vehicle Based on Incremental Nonlinear Dynamic InversionGuoming Chen0https://orcid.org/0000-0002-9153-7596An Liu1Junhua Hu2https://orcid.org/0000-0001-6128-0358Jinfu Feng3https://orcid.org/0000-0003-1265-9956Zongcheng Ma4https://orcid.org/0000-0001-5086-7540Aeronautics Engineering College, Air Force Engineering University, Xi’an, ChinaAeronautics Engineering College, Air Force Engineering University, Xi’an, ChinaAeronautics Engineering College, Air Force Engineering University, Xi’an, ChinaAeronautics Engineering College, Air Force Engineering University, Xi’an, ChinaSchool of Aviation Operations and Services, Aviation University of Air Force, Changchun, ChinaA vehicle able to navigate both in the air and underwater is referred to an unmanned aerial-underwater vehicle (UAUV). Aiming at the attitude and altitude control of UAUVs, an incremental dynamic inverse control (INDI) method with second-order low-pass filters is proposed. Based on the underwater motion model of an UAUV and the incremental attitude control model, the relationship between thrust increment and angular acceleration increment is obtained through Taylor series expansion and angular acceleration feedback. Subsequently, attitude and altitude controllers based on nonlinear dynamic inversion (NDI) and INDI are designed and their robustness is analyzed. By introducing second-order low-pass filters at the part of control and feedback, the accuracy of the angular acceleration estimation is improved and the time synchronization of the control system is ensured. Simulation results demonstrated that when introducing external disturbances and uncertainties, the INDI control with second-order low-pass filters proposed in this article can track the reference signal faster and more accurately than the NDI control.https://ieeexplore.ieee.org/document/9164924/Unmanned aerial-underwater vehicle (UAUV)incremental nonlinear dynamic inversion (INDI)attitude controlnonlinear dynamicslow-pass filter |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Guoming Chen An Liu Junhua Hu Jinfu Feng Zongcheng Ma |
spellingShingle |
Guoming Chen An Liu Junhua Hu Jinfu Feng Zongcheng Ma Attitude and Altitude Control of Unmanned Aerial-Underwater Vehicle Based on Incremental Nonlinear Dynamic Inversion IEEE Access Unmanned aerial-underwater vehicle (UAUV) incremental nonlinear dynamic inversion (INDI) attitude control nonlinear dynamics low-pass filter |
author_facet |
Guoming Chen An Liu Junhua Hu Jinfu Feng Zongcheng Ma |
author_sort |
Guoming Chen |
title |
Attitude and Altitude Control of Unmanned Aerial-Underwater Vehicle Based on Incremental Nonlinear Dynamic Inversion |
title_short |
Attitude and Altitude Control of Unmanned Aerial-Underwater Vehicle Based on Incremental Nonlinear Dynamic Inversion |
title_full |
Attitude and Altitude Control of Unmanned Aerial-Underwater Vehicle Based on Incremental Nonlinear Dynamic Inversion |
title_fullStr |
Attitude and Altitude Control of Unmanned Aerial-Underwater Vehicle Based on Incremental Nonlinear Dynamic Inversion |
title_full_unstemmed |
Attitude and Altitude Control of Unmanned Aerial-Underwater Vehicle Based on Incremental Nonlinear Dynamic Inversion |
title_sort |
attitude and altitude control of unmanned aerial-underwater vehicle based on incremental nonlinear dynamic inversion |
publisher |
IEEE |
series |
IEEE Access |
issn |
2169-3536 |
publishDate |
2020-01-01 |
description |
A vehicle able to navigate both in the air and underwater is referred to an unmanned aerial-underwater vehicle (UAUV). Aiming at the attitude and altitude control of UAUVs, an incremental dynamic inverse control (INDI) method with second-order low-pass filters is proposed. Based on the underwater motion model of an UAUV and the incremental attitude control model, the relationship between thrust increment and angular acceleration increment is obtained through Taylor series expansion and angular acceleration feedback. Subsequently, attitude and altitude controllers based on nonlinear dynamic inversion (NDI) and INDI are designed and their robustness is analyzed. By introducing second-order low-pass filters at the part of control and feedback, the accuracy of the angular acceleration estimation is improved and the time synchronization of the control system is ensured. Simulation results demonstrated that when introducing external disturbances and uncertainties, the INDI control with second-order low-pass filters proposed in this article can track the reference signal faster and more accurately than the NDI control. |
topic |
Unmanned aerial-underwater vehicle (UAUV) incremental nonlinear dynamic inversion (INDI) attitude control nonlinear dynamics low-pass filter |
url |
https://ieeexplore.ieee.org/document/9164924/ |
work_keys_str_mv |
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