2020 Vol. 46, No. 4

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Volume 46 Issue42020
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Real-time performance evaluation technology of airborne network for avionics system
HE Feng, ZHOU Xuan, ZHAO Changxiao, LI Qiao, WANG Peng, XIONG Huagang
2020, 46(4): 651-665. doi: 10.13700/j.bh.1001-5965.2019.0297
Abstract:

Airborne network is the key to realize real-time reliable transmission of information in avionics system. Its development degree and capability determine the overall configuration and comprehensive information efficiency of avionics system. Unlike general computer networks, airborne networks emphasi...

Separation technology of system noise in error motion test
FENG Ming, ZHOU Chengyu, ZHANG Kun, WANG Xinjie
2020, 46(4): 666-673. doi: 10.13700/j.bh.1001-5965.2019.0316
Abstract:

Since the error motion of the high-precision spindles is often in the same order as the noise of the test system, the measuring accuracy of the three-point method is greatly reduced by the noise signals. With the synchronous error motion (SEM), a combined processing algorithm with equal angle sampli...

Airline hub network optimization design under uncertain demand
LE Meilong, ZHENG Wenjuan, WU Minggong, WANG Zekun
2020, 46(4): 674-682. doi: 10.13700/j.bh.1001-5965.2019.0319
Abstract:

In order to help airlines plan route network reasonably and reduce operation cost, from the perspective of airlines, airport capacity is regarded as a function of arrival and departure flights to draw airport capacity envelope curve. Based on airport capacity envelope curve, a two-stage mixed intege...

Physics-based numerical simulation of AUV docking by self-propulsion
WU Lihong, WANG Shiwen, FENG Xisheng, LI Yiping, LIU Kaizhou
2020, 46(4): 683-690. doi: 10.13700/j.bh.1001-5965.2019.0305
Abstract:

To predict the effect of dock on hydrodynamic performance of autonomous underwater vehicle (AUV) and to improve AUV underwater docking success rate, a method of multi-block hybrid grids combined with dynamic layer method and user defined function (UDF) was presented, which was applied to the physics...

Terrain match aided navigation method of hypersonic glide vehicle
XIAN Yong, REN Leliang, YANG Zicheng, ZHANG Daqiao, LI Jie
2020, 46(4): 691-702. doi: 10.13700/j.bh.1001-5965.2019.0310
Abstract:

The height of the hypersonic vehicle gliding flight is over 30 km, so the atmosphere is extremely thin and the traditional terrain match aided navigation with barometric altimeter cannot work properly. In order to improve the accuracy of terrain match, on the basis of analyzing the insensitivity of ...

Path planning for mobile robot based on improved genetic algorithm
WEI Tong, LONG Chen
2020, 46(4): 703-711. doi: 10.13700/j.bh.1001-5965.2019.0298
Abstract:

Path planning is the key technology to realize autonomous navigation of mobile robots. For the problem that the path length is not the shortest and the path is not coherent in the two plan cycles with conventional path planning method, a new method for inter-frame correlation smooth path planning ba...

Video formatting method of near-space data for Web scientific visualization
TAN Jian, WANG Shenghua, GUO Changshun
2020, 46(4): 712-723. doi: 10.13700/j.bh.1001-5965.2019.0300
Abstract:

As a transitional region from sky to space, near-space has important value in the fields of science, economy and military. With the development of remote sensing technology and the continuous development of mode simulation, the massive near-space data of higher spatial and temporal resolution is inc...

Research on wagon-wheel fuel grain parametric design and internal ballistics performance of hybrid rocket motor
LI Xintian, CAI Qiang, LI Yancheng, WANG Xuekun, DAN Linpeng
2020, 46(4): 724-730. doi: 10.13700/j.bh.1001-5965.2019.0314
Abstract:

The study of fuel grain design and internal ballistic performance can provide the foundation for the design and optimization of hybrid rocket motor. Fuel grain design and internal ballistics calculation process and method of hybrid rocket motor were established. Based on the fuel regression rate law...

Inter-satellite communication rate control method of Beidou navigation constellation
LI Xianbin, WANG Jian, FAN Guangteng, YANG Zhixi
2020, 46(4): 731-738. doi: 10.13700/j.bh.1001-5965.2019.0411
Abstract:

Beidou navigation constellation can achieve autonomous orbit determination and performance enhancement by introducing inter-satellite ranging and transmitting links. During data transmission of inter-satellite links, the relative position change of satellites with time causes the constant change of ...

Interval interference time-variant reliability analysis method for propellant tank
XIN Tengda, ZHAO Jiguang, CUI Cunyan, DUAN Yongsheng
2020, 46(4): 739-745. doi: 10.13700/j.bh.1001-5965.2019.0294
Abstract:

During the service period of propellant tank, due to the existence of uncertain factors such as structural strength degradation and external random loads, the reliability of propellant tank is with time-variant characteristic. Based on interval theory and stress-strength interference theory, an inte...

Residual vibration suppression method of a cylindrical material loading robot
ZHENG Yu, GUANG Chenhan, YANG Yang
2020, 46(4): 746-753. doi: 10.13700/j.bh.1001-5965.2019.0296
Abstract:

In order to improve the material loading efficiency in vehicles, this paper proposes a new cylindrical material loading robot used in confined space. The residual vibration of the end-effector has been suppressed by optimizing the joint trajectory. Firstly, the overall design scheme and work flow of...

High-precision decoupling calibration method of multi-dimensional mounting spacecraft
MAO Boyuan, JI Junpeng, ZHANG Pengfei
2020, 46(4): 754-760. doi: 10.13700/j.bh.1001-5965.2019.0285
Abstract:

Aimed at the calibration problem of spacecraft multi-dimensional installation in the coupling situation, an on-orbit calibration method based on imager observation is proposed, and this method effectively overcomes the coupling nonlinearity of the calibration equations. Firstly, the geometric equati...

TSKF algorithm for pulsar position error estimation
XU Qiang, FAN Xiaohu, XU Liguo, WANG Hongli, FENG Lei
2020, 46(4): 761-768. doi: 10.13700/j.bh.1001-5965.2019.0288
Abstract:

In order to improve the robustness of the pulsar position error estimation to the proper motion and satellite position error and the efficiency of the overall algorithm, a two-stage Kalman filter (TSKF) algorithm is designed. Firstly, the influences of pulsar proper motion and satellite position err...

Formation control for high-order linear swarm systems with complex communication conditions
SHI Xiaohang, ZHANG Qingjie, LYU Junwei
2020, 46(4): 769-780. doi: 10.13700/j.bh.1001-5965.2019.0302
Abstract:

The formation control problems for high-order linear swarm systems with time-varying delays, topology uncertainties and external disturbances are investigated. Firstly, the mathematical description of the formation control for swarm systems is established, and the formation control protocol is propo...

Interval type-2 adaptive fuzzy sliding mode control design of reentry attitude for reusable launch vehicles
YANG Zhenshu, MAO Qi, DOU Liqian
2020, 46(4): 781-790. doi: 10.13700/j.bh.1001-5965.2019.0474
Abstract:

Considering the attitude tracking problem for reusable launch vehicles (RLVs) during reentry phase with high nonlinear and multi-variable coupling characteristics in the presence of parameter uncertainties and external disturbances, an interval type-2 adaptive fuzzy sliding mode based attitude contr...

High-precision geomagnetic reference map construction method based on compressed sensing
MA Xiaoyu, ZHANG Jinsheng, HAO Liangliang, LI Ting, WANG Shaobo, LI Lin
2020, 46(4): 791-797. doi: 10.13700/j.bh.1001-5965.2019.0313
Abstract:

The construction of geomagnetic reference map is the cornerstone of geomagnetic matching navigation.In this paper, the compressed sensing theory is applied to the geomagnetic information acquisition, which aims at solving the problem that the accuracy of the geomagnetic reference map is not satisfac...

Design and analysis of a 3-PPP compliant parallel micro-positioning stage
WANG Baoxing, MENG Gang, LIN Miao, LI Wei, CAO Yi
2020, 46(4): 798-807. doi: 10.13700/j.bh.1001-5965.2019.0286
Abstract:

The structure layouts of the existing spatial translational compliant parallel micro-positioning stages are not compact, and the parasitic motion of each kinematic joint accumulates during multi-axis actuation, which leads to the augment of cross-axis coupling error. In order to solve these problems...

A Cache design for image warping
KANG Jie, LIU Qiang
2020, 46(4): 808-813. doi: 10.13700/j.bh.1001-5965.2019.0284
Abstract:

The vehicle head-up display (HUD) system displays the source image plane on the windshield surface by image warping. Non-linear access to source image pixels degrades memory access efficiency. To solve this problem, a Cache is designed to ensure pixel access continuity, reduce memory access numbers ...

Research and design of synchronous GPS spoofing signal generation technology
LIU Yachuan, KOU Yanhong
2020, 46(4): 814-821. doi: 10.13700/j.bh.1001-5965.2019.0303
Abstract:

In order to meet the actual requirements of navigation spoofing of "low, slow, small" UAV, a miniaturized synchronous GPS spoofer has been developed based on our asynchronous GPS generator spoofer. Firstly, based on asynchronous GPS generator spoofer RF signal model, considering the spoofer signal p...

Rate-constrained traffic prediction of TTE network based on LSTM
SHI Yafei, LI Qiao, XIONG Huagang
2020, 46(4): 822-829. doi: 10.13700/j.bh.1001-5965.2019.0320
Abstract:

The rate constraint (RC) traffic in time triggered Ethernet (TTE) is event-triggered traffic. In the application scenario of dynamic scheduling of RC traffic, if it can predict the sequence of several RC traffic arriving at the switching node in a short time in the future, the switching node can mak...

Numerical study on mechanical properties of seaplane in whole water surface landing process
ZHAO Yunke, QU Qiulin, LIU Peiqing
2020, 46(4): 830-838. doi: 10.13700/j.bh.1001-5965.2019.0462
Abstract:

The numerical method is used to simulate the whole process of seaplane landing movement attitude and force, which is a complex problem combining water vapor two-phase flow, kinematics and dynamics. In this paper, the global motion grid method based on Fluent commercial software is combined with VOF ...