2018 Vol. 44, No. 3

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Volume 44 Issue32018
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Interactive multiple model filtering algorithm based on fuzzy logic
ZHOU Weidong, LIU Lu, TANG Jia
2018, 44(3): 413-419. doi: 10.13700/j.bh.1001-5965.2017.0160
Abstract:

The convergence speed and the filtering precision are poor when the interactive multiple model (IMM) filtering algorithm is applied to track the anti-ship missile in S maneuver. Thus a fuzzy logic interactive multiple model (FLIMM) filtering algorithm is proposed by improving the model probability u...

Discharge induced by plasma during high-velocity impact on target plate with gradient potential
TANG Enling, LIU Mei, HAN Yafei, WANG Ruizhi, HE Liping, LIU Shuhua
2018, 44(3): 420-428. doi: 10.13700/j.bh.1001-5965.2017.0203
Abstract:

Based on the objective reality of gradient potential existence in spacecraft surface caused by charged particles in space plasma environment in the orbiting spacecraft, discharge of spacecraft with surface charging or deep dielectric charging would be induced by debris or meteoroids impacting. In or...

Method for output displacement solving of compliant micro-motion mechanism with multi-input forces
GONG Jinliang, JIA Guopeng, ZHANG Yanfei
2018, 44(3): 429-436. doi: 10.13700/j.bh.1001-5965.2017.0219
Abstract:

For the compliant micro-motion mechanism with one input force, compliance describes the relation between output displacement and input force, and is an important performance index for the dynamic performance and positioning precision. For the one with many input forces, the relation equation between...

Failure behavior based storage life test design for inertial navigation products
XU Dan, LIN Kunsong, Chen Yunxia
2018, 44(3): 437-443. doi: 10.13700/j.bh.1001-5965.2017.0408
Abstract:

This paper proposed a failure-behavior-model based accelerated degradation test designing method for assessing the storage life of accelerometer for inertial navigation products, which determines test stress levels while lacking of the preliminary experimental data. On the basis of analyzing the pro...

Optical image enhancement method in dust environment on Mars
LI Haibo, CAO Yunfeng, DING Meng, ZHUANG Likui
2018, 44(3): 444-453. doi: 10.13700/j.bh.1001-5965.2017.0188
Abstract:

For dust impact on machine vision of the probe landing in Mars, a method was brought forward to remove the effect of dust on optical image and provide clear input image for the visual system. First, a model was built for the dust image. Then, the values of the atmospheric light and the transmission ...

Design method of cylindrical coil systems for generating uniform magnetic field
HU Zhaohui, MU Weiwei, WU Wenfeng, ZHOU Binquan
2018, 44(3): 454-461. doi: 10.13700/j.bh.1001-5965.2017.0152
Abstract:

In the field of precision measurement and aerospace, atomic gyroscope and atomic magnetometer have high requirements on the uniformity of magnetic field, while the uniformity of magnetic field generated by the traditional Helmholtz coil is not good enough for these applications. To obtain better fie...

Distributed coordinated navigation filtering algorithm for cooperative target by multi-satellite
LI Zhaoming, YANG Wenge, DING Dan, LIAO Yurong
2018, 44(3): 462-469. doi: 10.13700/j.bh.1001-5965.2017.0150
Abstract:

A distributed spherical simplex-radial cubature quadrature Kalman filter (DSSRCQKF) was proposed aiming at the coordinated navigation problem for cooperative target by multi-satellite on orbit. The spherical simplex rule and second-order Gauss-Laguerre quadrature rule were adopted to calculate the s...

High-efficiency solving method for steady transonic flow field
QIAO Lei, BAI Junqiang, QIU Yasong, HUA Jun, ZHANG Yang
2018, 44(3): 470-479. doi: 10.13700/j.bh.1001-5965.2017.0216
Abstract:

The implicit solving approach of steady transonic flow field equals a Newton iteration for a nonlinear equation system. Globalization of Newton iteration is usually necessary in practice in order to fulfill the convergence requirement. In the framework of homogenous continuation, a Laplace operator ...

Feedforward decoupling and internal model control for rotor of magnetically suspended control and sensing gyroscope
XIA Changfeng, CAI Yuanwen, REN Yuan, WU Dengyun, WANG Yingguang
2018, 44(3): 480-488. doi: 10.13700/j.bh.1001-5965.2017.0190
Abstract:

Magnetically suspended control and sensing gyroscope takes Lorentz force magnetic bearing (LFMB) as torquer to drive the rotor to tilt. As there is coupling between the two radial rotation degrees of freedom and it requires that rotor tilts with high precision and fast response, feedforward decoupli...

Path following of underactuated USV based on modified integral line-of-sight guidance strategies
CHEN Xiao, LIU Zhong, ZHANG Jianqiang, DONG Jiao, ZHOU Dechao
2018, 44(3): 489-499. doi: 10.13700/j.bh.1001-5965.2017.0192
Abstract:

Path following control is one of the key technologies for unmanned surface vehicle (USV) to complete its mission, which is widely concerned by the field of motion control at home and abroad. In order to improve the accuracy and robustness of USV's path following control under the disturbance of the ...

Response analysis of Timoshenko beam based on K-V damping model
ZHANG Xiayang, ZHU Ming, WU Zhe
2018, 44(3): 500-507. doi: 10.13700/j.bh.1001-5965.2017.0196
Abstract:

Based on Timoshenko beam theory, this paper has analyzed the dynamic properties when a clamped beam subjected to step load and moving load respectively. In addition, K-V damping model is considered to study the influence of damping on dynamic performance of the system. To acquire the theoretical sol...

Phase fluctuation noise adaptive cancellation system of superfluid gyroscope
ZHAO Yulong, SHEN Huairong, REN Yuan
2018, 44(3): 508-515. doi: 10.13700/j.bh.1001-5965.2017.0199
Abstract:

Aimed at the deterioration issue of gyroscope angular velocity measurement precision, which is caused by phase fluctuation noise of superfluid gyroscope, a gyroscope noise cancellation system based on recursive least square (RLS) algorithm was proposed. First, the phase detection model of superfluid...

Evaluation of directional ground stability and control characteristics in crosswind landing for civil airplane based on digital virtual flight
LIU Hailiang, WANG Lixin
2018, 44(3): 516-525. doi: 10.13700/j.bh.1001-5965.2017.0200
Abstract:

Based on airworthiness requirements of civil airplane, a method for evaluating ground stability and control of crosswind landing based on digital virtual flight is established. With maximum bank angle of airframe and maximum lateral deviation during the landing roll-out as key parameters, and in acc...

Vibration modal analysis of inflatable self-supporting booms
MA Ruiqiang, WEI Jianzheng, TAN Huifeng
2018, 44(3): 526-534. doi: 10.13700/j.bh.1001-5965.2017.0207
Abstract:

The inflatable self-supporting boom, which is made of laminated aluminum film and local discrete self-supporting thin shell, has the ability to support the effective load at zero inner pressure. In order to improve the accuracy predicting the vibration characteristics of the inflatable self-supporti...

A fault diagnosis model of plasticity echo state network based on L1/2-norm regularization
LU Cheng, XU Tingxue, WANG Hong
2018, 44(3): 535-541. doi: 10.13700/j.bh.1001-5965.2017.0214
Abstract:

In order to improve the dynamic adaptability of reservoir, overcome the ill-posed problems of output weights in echo state network (ESN), and balance the fitting and generalization ability, a fault diagnosis model of plasticity echo state network based on L1/2-norm regularization is presented. BCM r...

Optimization of aerostat helium temperature differences between day and night based on Kriging model
LIN Kang, MA Yunpeng, WU Zhe, WANG Qiang
2018, 44(3): 542-548. doi: 10.13700/j.bh.1001-5965.2017.0221
Abstract:

Considering the entire skin coating of aerostat envelop materials as one material, the effect of absorption and emission rate of aerostat envelop materials on helium temperature differences between day and night is investigated. In order to further reduce helium temperature differences between day a...

Harmonic timing sequence detection anti-jamming method and its implementation for FM fuze
KONG Zhijie, HAO Xinhong, LI Ping, YAN Xiaopeng
2018, 44(3): 549-555. doi: 10.13700/j.bh.1001-5965.2017.0224
Abstract:

In order to improve the anti-amplitude-modulation (AM)-jamming, anti-frequency-modulation (FM)-jamming and anti-sweep-jamming performance of FM fuze, a harmonic timing sequence detection anti-jamming method is proposed using the timing sequence characteristics of harmonics during the projectile-targ...

Terminal hypersonic trajectory modeling and optimization for maneuvering penetration and precision strike
LI Jinglin, CHEN Wanchun, MIN Changwan
2018, 44(3): 556-567. doi: 10.13700/j.bh.1001-5965.2017.0308
Abstract:

Aimed at the maneuvering penetration and precision strike problem of hypersonic vehicle terminal trajectory, an optimal maneuvering trajectory optimization method considering the dynamic characteristics of intercepting was proposed from the viewpoint of optimal control, so as to obtain the maximum m...

Kinematics analysis and multi-objective optimization of a novel parallel perfusion robot
YANG Hui, FANG Hairong, LI Dian, FANG Yuefa
2018, 44(3): 568-575. doi: 10.13700/j.bh.1001-5965.2017.0157
Abstract:

In order to meet the demand of honeycomb structure perfusion of large spacecraft, a novel hybrid perfusion robot is proposed. This article mainly focuses on the analysis of the parallel mechanism. First, the kinematics analysis of 3PSS-PU parallel mechanism is conducted, and the inverse kinematic mo...

A conflict detection algorithm for low-altitude flights based on SVM
HAN Dong, ZHANG Xuejun, NIE Zunli, GUAN Xiangmin
2018, 44(3): 576-582. doi: 10.13700/j.bh.1001-5965.2017.0159
Abstract:

With the continuous increasing of flight density, the aviation safety in low altitude has caused extensive concern. Low-altitude environment is complex, and ground obstacles and weather have more significant impact on low-altitude flight than commercial aviation. Traditional traffic alert and collis...

LPI radar signal recognition based on BDS-GD
WANG Xing, GUO Pengcheng, TIAN Yuanrong, WANG Yubing
2018, 44(3): 583-592. doi: 10.13700/j.bh.1001-5965.2017.0146
Abstract:

Regarding the deficiencies of bispectrum with big data and high dimension in signal feature extraction and recognition, a method combining bispectra diagonal slice (BDS) with generalized dimension (GD) was proposed. First, BDS was used to reduce data volume and GD in the multi-fractal theory was tak...

Reliability analysis of bus-based embryonic electronic array based on multi-state system
WANG Tao, CAI Jinyan, MENG Yafeng, ZHU Sai
2018, 44(3): 593-604. doi: 10.13700/j.bh.1001-5965.2017.0173
Abstract:

Through the analysis on structure characteristics and work principle of bus-based embryonic electronic array (BBEEA), the multi-state system theory is introduced to the reliability analysis of BBEEA, and the universal generating function (UGF) was used to model and analyze BBEEA reliability. Compare...

Impact time control guidance law for large heading errors
WANG Bin, LEI Humin, LI Jiong, YE Jikun, LI Ningbo
2018, 44(3): 605-613. doi: 10.13700/j.bh.1001-5965.2017.0162
Abstract:

In order to achieve salvo attack for large heading errors with integrated time, an impact time control guidance (ITCG) law for large heading errors is proposed based on equivalent sliding mode control theory and Lyapunov stability theorem by adopting the nonlinear guidance equation and the time-to-g...

Stability analysis of explorer in soft landing mode of engine shutdown at touchdown
DING Zongmao, WANG Chunjie, WU Hongyu, DING Jianzhong, GUO Fan
2018, 44(3): 614-620. doi: 10.13700/j.bh.1001-5965.2017.0194
Abstract:

The soft landing stability will be greatly reduced if the main engine of planetary explorer fails to shut down timely. In order to avoid this reduction, a new shutdown mode is introduced to serve as a remedy where engine is shut down at touchdown. The dynamic model of the explorer equiped with novel...

Fault fusion diagnosis of aero-engine based on deep learning
CHE Changchang, WANG Huawei, NI Xiaomei, HONG Jiyu
2018, 44(3): 621-628. doi: 10.13700/j.bh.1001-5965.2017.0197
Abstract:

Through the fault diagnosis of aero-engine, the working status of each component can be correctly judged, and the maintenance program can be determined quickly to ensure the safety of flight. Based on the combination of deep belief network and decision fusion theory, the fault fusion diagnosis model...

Spares transshipment strategy analysis based on a three-site inventory system
XUE Pei, WANG Naichao, XIAO Boping, MA Lin
2018, 44(3): 629-635. doi: 10.13700/j.bh.1001-5965.2017.0212
Abstract:

In this paper, the effect of variant transshipment strategies on expected backorders (EBO) of a three-site inventory system is researched. Based on the predefined assumptions and inventory control strategy, as well as the consumption and replenishment process of the spares, the state equations of sp...

Adaptive threshold zero-velocity update algorithm under multi-movement patterns
ZHANG Jianmin, XIU Chundi, YANG Wei, YANG Dongkai
2018, 44(3): 636-644. doi: 10.13700/j.bh.1001-5965.2017.0148
Abstract:

Zero-velocity update (ZUPT) algorithm is imported to calibrate device's cumulative error in traditional inertial navigation system (INS) which is based on micro-electro-mechanical system inertial mea-surement unit (MEMS-IMU). The positioning accuracy will be reduced when the movement trajectory of i...

A method for branch identification of planar six-bar linkages with sliding pairs
GONG Yajing, WANG Jun, WANG Quan, BI Shusheng, REN Jun, SUN Jinfeng
2018, 44(3): 645-652. doi: 10.13700/j.bh.1001-5965.2017.0151
Abstract:

The identification of branch, motion defect and range of motion of the planar six-bar linkages with sliding pairs is an important indicator for motion characteristics of linkages. Firstly, this paper divides the planar six-bar linkages with two sliding pairs or three sliding pairs into four-bar chai...