Shenmin Song

Prof. Shenmin Song

orcid

Research Focus & Metrics

Academic Career Length

21Years (2006-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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11 February 2016 in International Journal of Control, Automation, and Systems
Verified
Journal Article
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JSJunhong Song
Junhong Song
SSShenmin Song
Shenmin Song
HZHuibo Zhou
Huibo Zhou

17 January 2018 in International Journal of Control, Automation, and Systems
Verified
Journal Article
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HCHai-Tao Chen
Hai-Tao Chen
SSShenmin Song
Shenmin Song
ZZZhi-Bin Zhu
Zhi-Bin Zhu

8 November 2022 in IEEE Sensors Journal
Verified
Journal Article
Closed access
YYYahu Yang
Yahu Yang
XGXiangzhou Gao
Xiangzhou Gao
YWYu Wang
Yu Wang
SSShenmin Song
Shenmin Song
Unmanned aerial vehicles (UAVs) have been widely used in various fields. As one of the key technologies in improving the autonomous sensing ability of UAV optical sensors, object detection has become a research focus in recent years. Since UAVs usually navigate at different vertical heights, the object scales and sensor field of view change violently, which brings a great difficulty to the optimization of the model. Moreover, when a UAV is flying at low level rapidly, it may cause the motion blur phenomenon on objects that are highly dense in position, leading to great challenge for distinction of these objects. To address the extremely tough problems discussed above, we propose an accurate and efficient object detection algorithm, namely VAMYOLOX. Based on YOLOX, we first redesigned the classification and regression loss function of the model to better conduct classification and localization under complex motion blur and dense scenes. Then we increase another prediction head to detect lots of tiny objects to ultimately improve the detection ability of the model for multi-scale objects. Finally, we redesigned the neck of the network by introducing the triplet attention module (TAM) to find attention regions in scenes with dense objects and in images that cover a large area, accordingly enhancing the features extracted by the backbone network. Extensive experiments on dataset VisDrone widely used in the research of UAV image object detection show that VAMYOLOX has achieved state-of-the-art (SOTA) performance with good interpretability in UAV optical sensors captured scenes. On VisDrone-DET-test-dev subset, the average precision (AP) of VAMYOLOX is 25.31%, outperforming the previous SOTA model (CornerNet) by 1.88%. On VisDrone-DET-val subset, the AP of our method is 29.4%, achieving highly competitive result with previous SOTA method (AMRNet). Not only that, VAMYOLOX achieves a maximum improvement of 2.72% compared to the AP of the baseline model (YOLOX). In addition, compared with other methods, our method has a significant advantage in speed and can meet the needs of different scenarios. The PyTorch code and trained models are available at https://github.com/yangyahu-1994/VAMYOLOX.

26 September 2015 in International Journal of Control, Automation, and Systems
Verified
Journal Article
Closed access
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YGYong Guo
Yong Guo
SSShenmin Song
Shenmin Song
XLXue-Hui Li
Xue-Hui Li

2 January 2018 in Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Verified
Journal Article
Closed access
XLXuehui Li
Xuehui Li
ZZZhibin Zhu
Zhibin Zhu
SSShenmin Song
Shenmin Song
In this paper, the problem of autonomous rendezvous and docking with a non-cooperative target spacecraft is studied. A coupled translational and rotational dynamics of the spacecraft is used, where the rotation matrix is used to represent the attitude of spacecraft to overcome the drawbacks related to the unwinding. An asymptotically stable autonomous rendezvous and docking collision-free controller is proposed based on a novel designed sliding surface. Then, a new nonsingular terminal sliding surface is given, based on which the developed autonomous rendezvous and docking collision-free controller can make the tracking errors converge into a small bounded area near the origin in a finite time. Using artificial potential function and virtual obstacles model established based on cissoid, both controllers ensure the chaser spacecraft strictly remains in the safety area to avoid the collision with the target spacecraft. The effectiveness of the proposed controllers is demonstrated by numerical simulation.

17 April 2018 in Nonlinear Dynamics
Verified
Journal Article
Closed access
PDF file
XLXuehui Li
Xuehui Li
SSShenmin Song
Shenmin Song
YGYong Guo
Yong Guo