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Dynamical analysis and validation of motion control by filtering performance for aerial robotic system

Authors :
Anh Son Tran
Anh Huy Vo
Diep Cong Thanh Tu
Ha Quang Thinh Ngo
Source :
Journal of Vibroengineering, Vol 23, Iss 6, Pp 1456-1475 (2021)
Publication Year :
2021
Publisher :
JVE International Ltd., 2021.

Abstract

Although drone appears in different applications, such as environmental inspection, agriculture or transportation, some aspects require more studies to clarify the efficient outcomes. One of them is to investigate the filtering performance such as Kalman and Complementary filters when the autonomous aerial system (AAS) handles its mission. However, it lacks the systematic research about these filters to provide the proper evaluation. Therefore, in this paper, the research topic related to AAS model to indicate the filtering effects in the agricultural application for making an alternative solution is presented. Firstly, the mathematical representation of system model is established in order to describe the dynamical performance and motion constraints. Then, the theory of filter structure is implemented to estimate the system state. The proposed design is validated in both numerical simulation and experiments. The system parameters that are monitored, include angular values of roll, pitch and yaw in three axes, motion parameters and its trajectories. By utilizing various sensing devices such as gyroscope, accelerometer and compass in real-world hardware, the experimental results could evaluate more precise and efficient design. The findings of this study are to (1) propose the model of AAS and proper filters, (2) launch the verified process and calibration, and (3) demonstrate the competitive performance among filters. From these results of our work, it could be clearly seen that the AAS plays an important role in daily applications and the related topics are still attractive.

Details

ISSN :
25388460 and 13928716
Volume :
23
Database :
OpenAIRE
Journal :
Journal of Vibroengineering
Accession number :
edsair.doi.dedup.....3623a99f848d8b3d37f9262327761080