• Title/Summary/Keyword: aeronautics

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High-Pass-Filter-Based Virtual Impedance Control for LCL-filtered Inverters Under Weak Grid

  • Wang, Jiangfeng;Xing, Yan;Zhang, Li;Hu, Haibing;Yang, Tianyu;Lu, Daorong
    • Journal of Power Electronics
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    • v.18 no.6
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    • pp.1780-1790
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    • 2018
  • Voltage feed-forward control (VFFC) is widely used in LCL-type grid-tied inverters due to its advantages in terms of disturbance rejection performance and fast dynamic response. However, VFFC may worsen the stability of inverters under weak grid conditions. It is revealed in this paper that a large phase-lag in the low-frequency range is introduced by VFFC, which reduces the phase margin significantly and leads to instability. To address this problem, a novel virtual-impedance-based control, where a phase-lead is introduced into the low-frequency area to compensate for the phase lag caused by VFFC, is proposed to improve system stability. The proposed control is realized with a high-pass filter, without high-order-derivative components. It features easy implementation and good noise immunity. A detailed design procedure for the virtual impedance control is presented. Both theoretical analysis and experimental results verify the effectiveness of the control proposed.

Fast-convergence trilinear decomposition algorithm for angle and range estimation in FDA-MIMO radar

  • Wang, Cheng;Zheng, Wang;Li, Jianfeng;Gong, Pan;Li, Zheng
    • ETRI Journal
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    • v.43 no.1
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    • pp.120-132
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    • 2021
  • A frequency diverse array (FDA) multiple-input multiple-output (MIMO) radar employs a small frequency increment across transmit elements to produce an angle-range-dependent beampattern for target angle and range detection. The joint angle and range estimation problem is a trilinear model. The traditional trilinear alternating least square (TALS) algorithm involves high computational load due to excessive iterations. We propose a fast-convergence trilinear decomposition (FC-TD) algorithm to jointly estimate FDA-MIMO radar target angle and range. We first use a propagator method to obtain coarse angle and range estimates in the data domain. Next, the coarse estimates are used as initialized parameters instead of the traditional TALS algorithm random initialization to reduce iterations and accelerate convergence. Finally, fine angle and range estimates are derived and automatically paired. Compared to the traditional TALS algorithm, the proposed FC-TD algorithm has lower computational complexity with no estimation performance degradation. Moreover, Cramer-Rao bounds are presented and simulation results are provided to validate the proposed FC-TD algorithm effectiveness.

Deeper SSD: Simultaneous Up-sampling and Down-sampling for Drone Detection

  • Sun, Han;Geng, Wen;Shen, Jiaquan;Liu, Ningzhong;Liang, Dong;Zhou, Huiyu
    • KSII Transactions on Internet and Information Systems (TIIS)
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    • v.14 no.12
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    • pp.4795-4815
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    • 2020
  • Drone detection can be considered as a specific sort of small object detection, which has always been a challenge because of its small size and few features. For improving the detection rate of drones, we design a Deeper SSD network, which uses large-scale input image and deeper convolutional network to obtain more features that benefit small object classification. At the same time, in order to improve object classification performance, we implemented the up-sampling modules to increase the number of features for the low-level feature map. In addition, in order to improve object location performance, we adopted the down-sampling modules so that the context information can be used by the high-level feature map directly. Our proposed Deeper SSD and its variants are successfully applied to the self-designed drone datasets. Our experiments demonstrate the effectiveness of the Deeper SSD and its variants, which are useful to small drone's detection and recognition. These proposed methods can also detect small and large objects simultaneously.

A Variational Framework for Single Image Dehazing Based on Restoration

  • Nan, Dong;Bi, Du-Yan;He, Lin-Yuan;Ma, Shi-Ping;Fan, Zun-Lin
    • KSII Transactions on Internet and Information Systems (TIIS)
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    • v.10 no.3
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    • pp.1182-1194
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    • 2016
  • The single image dehazing algorithm in existence can satisfy the demand only for improving either the effectiveness or efficiency. In order to solve the problem, a novel variational framework for single image dehazing based on restoration is proposed. Firstly, the initial atmospheric scattering model is transformed to meet the kimmel's Retinex variational model. Then, the green light component of image is considered as an input of the variational framework, which is generated by the sensitivity of green wavelength. Finally, the atmospheric transmission map is achieved by multi-resolution pyramid reduction to improve the visual effect of the results. Experimental results demonstrate that the proposed method can remove haze effectively with less memory consumption.

Numerical study of flow of Oldroyd-3-Constant fluids in a straight duct with square cross-section

  • Zhang, Mingkan;Shen, Xinrong;Ma, Jianfeng;Zhang, Benzhao
    • Korea-Australia Rheology Journal
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    • v.19 no.2
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    • pp.67-73
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    • 2007
  • A finite volume method (FVM) base on the SIMPLE algorithm as the pressure correction strategy and the traditional staggered mesh is used to investigate steady, fully developed flow of Oldroyd-3-constant fluids through a duct with square cross-section. Both effects of the two viscoelastic material parameters, We and ${\mu}$, on pattern and strength of the secondary flow are investigated. An amusing sixteen vortices pattern of the secondary flow, which has never been reported, is shown in the present work. The reason for the changes of the pattern and strength of the secondary flow is discussed carefully. We found that it is variation of second normal stress difference that causes the changes of the pattern and strength of the secondary flow.

The Model Driven Development of the Multi-function Display Software for Avionics (모델 기반 항공기 다중 시현기 소프트웨어의 개발)

  • Yoo, Hongseok;Hwang, Dong Gil;Kim, So Yong;Park, Ye Chan;Park, Seong Hun
    • Proceedings of the Korean Society of Computer Information Conference
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    • 2017.07a
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    • pp.413-414
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    • 2017
  • 항공전자 시스템 및 소프트웨어 기술의 복잡성이 증가함에 따라 소프트웨어의 신뢰성을 보장하는 방법으로 모델 기반 소프트웨어 개발의 필요성이 증가하고 있다. 본 논문에서는 모델기반 소프트웨어 설계를 이용하여 항공기 콕핏 내 주요 계기를 통합한 MFD(Multi-function Display)를 설계하고, 실시간 비행 데이터를 생성하여 시뮬레이션한 결과를 보인다.

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Multi-information fusion based localization algorithm for Mars rover

  • Jiang, Xiuqiang;Li, Shuang;Tao, Ting;Wang, Bingheng
    • Advances in aircraft and spacecraft science
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    • v.1 no.4
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    • pp.455-469
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    • 2014
  • High-precision autonomous localization technique is essential for future Mars rovers. This paper addresses an innovative integrated localization algorithm using a multiple information fusion approach. Firstly, the output of IMU is employed to construct the two-dimensional (2-D) dynamics equation of Mars rover. Secondly, radio beacon measurement and terrain image matching are considered as external measurements and included into the navigation filter to correct the inertial basis and drift. Then, extended Kalman filtering (EKF) algorithm is designed to estimate the position state of Mars rovers and suppress the measurement noise. Finally, the localization algorithm proposed in this paper is validated by computer simulation with different parameter sets.

Aerodynamic Design of a Novel Low-Reynolds-Number Airfoil for Near Space Propellers

  • Zhang, Shunlei;Yang, Xudong;Song, Bifeng;Song, Wenping
    • International Journal of Aerospace System Engineering
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    • v.2 no.1
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    • pp.53-57
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    • 2015
  • For improving the efficiency of near space propellers working over 20km, performances of their streamwise sections, i.e. low-Reynolds-number airfoils which work at $10^4-10^5$ Reynolds numbers, are significant. Based on the low-Reynolds-number CFD technology, this paper designs a novel low-Reynolds-number airfoil. Unsteady characteristics of the laminar separation bubble on novel airfoil and a typical conventional airfoil are studied numerically, and the Reynolds number effect is investigated. Results show that at $10^4-10^5$ Reynolds numbers, unsteady aerodynamic characteristics of the novel airfoil are severely weakened and its lift-to-drag ratio can increase about 100%.

Structural Design of Composite Blade and Tower for Small Wind Turbine System

  • Jang, Mingi;Lee, Sanggyu;Park, Gwanmun;Park, Hyunbum
    • International Journal of Aerospace System Engineering
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    • v.2 no.1
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    • pp.38-42
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    • 2015
  • This work is to propose a structural design and analysis procedure for development of the low noise 1kW class small wind turbine system which will be applicable to relatively low speed region like Korea and for the domestic use. The proposed structural configuration has a sandwich composite structure with the E-glass/Epoxy face sheets and the Urethane foam core for lightness, structural stability, low manufacturing cost and easy manufacturing process. Structural analysis including load cases, stress, deformation, buckling, vibration and fatigue life was performed using the Finite Element Method, the load spectrum analysis and Miner rule. In order to evaluate the designed structure, the structural test was carried out and its test results were compared with the estimated results. Moreover Investigation on structural safety of tower was verified through structural analysis by FEM.