2018 Vol. 44, No. 4

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Nonlinear vibration response characteristics of high-speed flexible rotor system
HONG Jie, YU Huan, XIAO Sen, MA Yanhong
2018, 44(4): 653-661. doi: 10.13700/j.bh.1001-5965.2017.0266
Abstract:

According to the multi-supported structure feature of high-speed flexible rotor and with the demand of rotor dynamic design, the influence of the bearing looseness on the rotor dynamic was analyzed. The nonlinear vibration response characteristics of the high-speed flexible rotor system were obtaine...

Power matching of flying cars during takeoff stage based on dual-mode driving
XU Bin, TIAN Fugang
2018, 44(4): 662-669. doi: 10.13700/j.bh.1001-5965.2017.0279
Abstract:

To solve power-matching problem during takeoff stage of folding wing flying car, the basic dynamic control strategy was studied.The dual-mode driving characteristics during takeoff stage were analyzed through theoretical calculation, and the concept of the optimal switching time was proposed.Based o...

Fast acquisition methods based on sparse Fourier transform
ZHANG Chunxi, LI Xianmu, GAO Shuang
2018, 44(4): 670-676. doi: 10.13700/j.bh.1001-5965.2017.0280
Abstract:

The acquisition of the satellite signals is the key step of baseband signal processing in the receiver. The speed of the acquisition has a serious effect on the time to first fix (TTFF).According to the parallel code phase search (PCPS) method based on fast Fourier transform (FFT), the sparse Fourie...

Influence of meteorological factors on aircraft fuel efficiency in approach flight
HU Rong, WU Wenjie, CHEN Lin, ZHANG Feifei
2018, 44(4): 677-683. doi: 10.13700/j.bh.1001-5965.2017.0245
Abstract:

Meteorological factors are significant to aviation flight. To investigate the fuel efficiency in aviation flight, base of aircraft data (BADA) model was combined with meteorological factors, and the aircraft fuel consumption correction model was built. Taking the example of one inbound flight approa...

BDS/GPS combined navigation receiver autonomous integrity monitoring algorithm
WANG Ershen, YANG Fuxia, PANG Tao, QU Pingping, LAN Xiaoyu, JIANG Yi
2018, 44(4): 684-690. doi: 10.13700/j.bh.1001-5965.2017.0277
Abstract:

In order to make receiver autonomous integrity monitoring (RAIM) technique be applied to approach with vertical guidance (APV) flight phase in civil aviation navigation, the BDS/GPS combined navigation RAIM algorithm is studied. An algorithm based on the optimal weighted average solution of BDS/GPS ...

Kinematic and mechanical analysis on launch process of stratospheric airship
ZHANG Taihua, JIANG Luhua, ZHOU Jianghua
2018, 44(4): 691-699. doi: 10.13700/j.bh.1001-5965.2017.0227
Abstract:

Launch mode of the stratospheric airship is the prerequisite factor to safely reach the target altitude. In this paper, a dynamics model for the launch process of stratospheric airship is firstly established, and the analytical solution method is put forward, and the quantitative analysis is carried...

Joint optimization of detection and tracking with Rao-Blackwellized Monte Carlo data association
CHEN Weishi, YAN Jun, LI Jing
2018, 44(4): 700-708. doi: 10.13700/j.bh.1001-5965.2017.0228
Abstract:

A joint optimization algorithm was proposed for radar target detection and tracking with Rao-Blackwellized Monte Carlo data association. Rao-Blackwellization made the separation of single target tracking and data association, where the data association was solved by the sequential Monte Carlo method...

Influence mechanism of axial spacing on rotor blade flutter characteristics
ZHENG Yun, YU Yongbo
2018, 44(4): 709-716. doi: 10.13700/j.bh.1001-5965.2017.0251
Abstract:

The mechanism of the upstream blade row affecting the flutter characteristics of the rotor blade is studied, using the self-developed unsteady fluid-solid coupling numerical simulation program. The influence coefficient method is used to analyze the effect of axial spacing on the aeroelastic stabili...

Design of decoupling controller for spinning missile based on receding horizon optimization
CHEN Wei, SUN Chuanjie, FENG Gaopeng, BAI Yunshan
2018, 44(4): 717-724. doi: 10.13700/j.bh.1001-5965.2017.0271
Abstract:

The spinning missiles are subjected to external disturbances and uncertainties during flight, and there are the aerodynamic cross-linking, inertial cross-linking and control cross-linking. To realize stable flight, it is necessary to design decoupling controller. Therefore, a decoupling control meth...

Equipment RUL prediction oriented parallel simulation technology
GE Chenglong, ZHU Yuanchang, DI Yanqiang
2018, 44(4): 725-736. doi: 10.13700/j.bh.1001-5965.2017.0262
Abstract:

As an emerging simulation technology in the field of system modeling & simulation, equipment parallel simulation has become research emphasis. In the field of equipment maintenance support, the outstanding problem of equipment remaining useful life(RUL) prediction is analyzed, i.e., the stable m...

Adaptive sliding mode control of solar array with input shaping
ZHOU Tong, GUO Hong, XU Jinquan
2018, 44(4): 737-745. doi: 10.13700/j.bh.1001-5965.2017.0276
Abstract:

This paper proposes a control strategy which combines adaptive sliding mode control (ASMC) with input shaping technology for the solar array drive system (SADS) to improve the angular position control performance and suppress the flexible vibration. To improve the angular position control performanc...

Modular design method for filament winding machine
XU Xiaoming, ZHANG Wuxiang, DING Xilun
2018, 44(4): 746-758. doi: 10.13700/j.bh.1001-5965.2017.0233
Abstract:

Winding machine is the core equipment for filament winding with the features of high production efficiency and stable product quality. To meet the requirements of customized and small batch production, the modular design method (MDM) is proposed to expand the function of winding machine. The system ...

Effect of planet's third-body gravitational perturbation on aerobraking of moon's explorer
JIANG Ling, WANG Yue, XU Shijie
2018, 44(4): 759-764. doi: 10.13700/j.bh.1001-5965.2017.0249
Abstract:

An averaged orbital dynamics model for a natural satellite aerobraking was established and an Titan explorer was simulated to study the notable planet's third-body gravitational perturbation during the process. Firstly, non-singular Milankovitch elements were introduced to represent the orbital moti...

Experimental analysis of carbon dioxide diffusion coefficient in RP-3 jet fuel
LI Chaoyue, FENG Shiyu, SHAO Lei, PAN Jun, LIU Weihua
2018, 44(4): 765-771. doi: 10.13700/j.bh.1001-5965.2017.0265
Abstract:

The rule of mass diffusion of CO2 in jet fuel is an important consideration in the research of the aircraft fuel tank inerting system. A pressure-decay test apparatus was constructed to measure the diffusion coefficient of carbon dioxide in RP-3 jet fuel by monitoring the pressure variation at const...

Exploring LSTM based recurrent neural network for failure time series prediction
WANG Xin, WU Ji, LIU Chao, YANG Haiyan, DU Yanli, NIU Wensheng
2018, 44(4): 772-784. doi: 10.13700/j.bh.1001-5965.2017.0285
Abstract:

Effectively forecasting the failure data in the usage stage is essential to reasonably make reliability plans and carry out reliability maintaining activities. Beginning with the historical failure data of complex system, a long short-term memory (LSTM) based recurrent neural network for failure tim...

Frequency extension method of TEM cells based on slotted waveguide antenna
SONG Chunjiang, FENG Xiaoyao, DAI Fei
2018, 44(4): 785-791. doi: 10.13700/j.bh.1001-5965.2017.0296
Abstract:

In order to break through limitatiions in actual testing, the extension method of frequency range of a transverse electromagnetic (TEM) cell is studied. Using the theory of electromagnetic field and microwave technology, the influence of adding slots to the cell on the higher order modes is analyzed...

Multicore design space exploration via semi-supervised ensemble learning
LI Dandan, YAO Shuzhen, WANG Ying, WANG Senzhang, TAN Huobin
2018, 44(4): 792-801. doi: 10.13700/j.bh.1001-5965.2017.0297
Abstract:

With the increasing complexity of microprocessor architecture, the design space is growing exponentially and the software simulation technology is extremely time-consuming. Design space exploration becomes one major challenge when processors are designed. The paper proposed an efficient design space...

Multiple fault diagnosis and maintenance strategy based on testability D matrix
TIAN Heng, DUAN Fuhai, FAN Liang, SANG Yong, SHI Meng
2018, 44(4): 802-809. doi: 10.13700/j.bh.1001-5965.2017.0225
Abstract:

In view of the complicated multiple fault diagnosis problems and difficulties in the realization of multiple fault direct processing algorithm, on the basis of testability D matrix and single fault algorithm, a novel multiple fault diagnosis and maintenance strategy based on translating into single ...

Computation method of collision probability of space object based on Laplace transformation
HUO Yurong, LI Zhi, HAN Lei
2018, 44(4): 810-819. doi: 10.13700/j.bh.1001-5965.2017.0263
Abstract:

The collision probability of space object is an important information for judging whether a collision occurs in the space debris collision warning, and is important for the maneuvering avoidance of the spacecraft. Based on the Laplace transformation and the definition of the power series, the collis...

Moon-based platform data transmission link scheme design and analysis
CHEN Guoqiang, RUAN Zhixing, GUO Huadong, LIU Guang, DING Yixing, ZHANG Yanxin
2018, 44(4): 820-827. doi: 10.13700/j.bh.1001-5965.2017.0290
Abstract:

The ability of data transmission and processing is an important factor in the construction of the moon-based platform. How to transmit the observation data to the earth station efficiently and accurately is a critical step to carry out the further researches. Through the joint simulation of STK and ...

Improved flower pollination algorithm for multimodal function optimization
GUO Qing, HUI Xiaobin, ZHANG Jiakui, LI Zhengxin
2018, 44(4): 828-840. doi: 10.13700/j.bh.1001-5965.2017.0240
Abstract:

In order to discuss the defects of flower pollination algorithm (FPA) in solving multimodal optimization problems, the optimal disadvantages of flower pollination algorithm in multimodal function optimization were qualitatively analyzed by defining population diversity and difference index. And then...

Formation reconfiguration control of quadrotor UAVs based on adaptive communication topology
MA Siqian, DONG Chaoyang, MA Mingyu, WANG Qing
2018, 44(4): 841-850. doi: 10.13700/j.bh.1001-5965.2017.0281
Abstract:

This paper focuses on the cooperative control problem in formation reconfiguration of multiple flight vehicles, and the method of integral sliding mode control (ISMC) based on switching communication topology is investigated. The multiple flight vehicle system is modeled involving the connecting of ...

Octree based decimation algorithm for triangle isosurface using simplified patterns
XU Lei, WANG Huafeng, PAN Haixia, LIN Guangyan, CHEN Yuexi
2018, 44(4): 851-861. doi: 10.13700/j.bh.1001-5965.2017.0282
Abstract:

It is universally acknowledged that SMC based on simplified patterns extracts less triangles than the standard MC. Because only in-cube decimation was exploited, SMC is not able to take full advantage of local features of isosurfaces. Based on this observation, a new method named OSMC is presented i...

Interaction between metallic and nonmetallic elements on grain boundary of nickel
FANG Shujuan, SHI Songxin, ZHU Linggang, ZHOU Jian
2018, 44(4): 862-867. doi: 10.13700/j.bh.1001-5965.2017.0293
Abstract:

First-principles calculations based on density functional theory are used to study the segregation of metallic and nonmetallic elements as well as their interactions on the grain boundary (GB) of nickel. Two typical GBs are constructed:close-packed GB and quite open GB. According to the solution ene...

Synthesis and characterization of high purity V2AlC prepared by pressureless sintering
GAO Shaohua, MIAO Naihua, ZHOU Jian
2018, 44(4): 868-873. doi: 10.13700/j.bh.1001-5965.2017.0295
Abstract:

In this paper, we reported the synthesis of high purity V2AlC by pressureless sintering with V, Al and C mixed powders. The reaction paths were studied and discussed according to the phase transformation at different sintering temperatures. Besides, the effect of sintering aid NaF on singtering proc...

Preparation and tribological properties of Zn-Cr2AlC composites
LI Zhi, ZHAO Wenyue, MIAO Naihua
2018, 44(4): 874-878. doi: 10.13700/j.bh.1001-5965.2017.0298
Abstract:

In order to improve the friction and wear properties of Zn, Cr2AlC ceramic particle reinforced Zn matrix composites were prepared by hot pressing method. The effects of Cr2AlC content on the metallographic structure, Vickers-hardness, relative density and tribological properties of the Zn-based comp...

Immunological response evaluation of absorbable collagen membrane in vivo
ZHANG Lin, SUN Lei, XU Menghan, NIU Xufeng
2018, 44(4): 879-886. doi: 10.13700/j.bh.1001-5965.2017.0230
Abstract:

Immune response is one of the critical factors to limit implantable biomaterials' application. In this study, two kinds of collagen membranes for bone regeneration were evaluated in terms of immunological response in vivo, which is hoped to lay foundations for clinical trials. At day 14 following su...

Multi-objective reliability design optimization approach based on competition game
FENG Jiazhen, ZHANG Jianguo, QIU Jiwei
2018, 44(4): 887-894. doi: 10.13700/j.bh.1001-5965.2017.0367
Abstract:

Aimed at the subjectivity of the selection of target weights, multi-objective reliability design optimization approach based on competition game is proposed. In this approach, every design objective is treated as the corresponding game player, and the random design variable set is decomposed into mu...