2017 Vol. 43, No. 6

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Spacecraft attitude passivity control based on PCH model
WANG Qing, GONG Ligang, DONG Chaoyang
2017, 43(6): 1061-1071. doi: 10.13700/j.bh.1001-5965.2016.0414
Abstract:

For the spacecraft attitude control problem in the presence of disturbance torques, a passivity control scheme based on port-controlled Hamiltonian (PCH) system model was proposed from the perspective of energy. By writing the attitude control system in a PCH form and adding the state related to int...

Imperative modeling elements for multi-rotor unmanned aerial vehicles
WAN Jia, LIU Hong, WANG Fuxin
2017, 43(6): 1072-1079. doi: 10.13700/j.bh.1001-5965.2016.0481
Abstract:

The multi-rotor unmanned aerial vehicle (UAV) is one of the popular configurations in the UAV industry for small UAVs. However, research on the modeling of multi-rotor vehicles and its characteristics regarding flight mechanics is still limited. A flight mechanics model for multi-rotor UAV is develo...

Hardened test method of structural reliability based on correlation analysis
MA Xiaobing, ZHANG Jianchun, ZHAO Yu
2017, 43(6): 1080-1084. doi: 10.13700/j.bh.1001-5965.2016.0420
Abstract:

The traditional test verification of structural reliability is generally based on the independence assumption between loading stress and structural strength. Stating with the correlation analysis of stress and strength, we propose a hardened test method of structural reliability verification based o...

Comparison between external store separation and buried store separation of fighter
ZHANG Qunfeng, YAN Panpan, LI Jun
2017, 43(6): 1085-1097. doi: 10.13700/j.bh.1001-5965.2016.0497
Abstract:

To analyze the difference between external store separation and buried store separation, several separation cases were simulated using the same missile under the conditions of both subsonic and supersonic inflow. Improved delayed detached eddy simulation (IDDES) method based on Menter SST turbulence...

Active flutter suppression design of a wing based on sliding mode observer
SONG Chen, WANG Shiqi, YANG Chao
2017, 43(6): 1098-1104. doi: 10.13700/j.bh.1001-5965.2016.0453
Abstract:

Active flutter suppression (AFS) is a worldwide well proposed solution for the flutter of aircraft, which plays an important role in modern aircraft design. Many studies have shed some light on the AFS usage of sliding mode control strategy and the sliding mode observer, acting on two-dimensional wi...

A haze removal method for unmanned aerial vehicle images based on robust estimation of atmospheric light
LIU Chunhui, QI Yue, DING Wenrui
2017, 43(6): 1105-1111. doi: 10.13700/j.bh.1001-5965.2016.0473
Abstract:

Aimed at the problem that the quality of the images acquired by unmanned aerial vehicle (UAV) is easily reduced due to the fog or haze weather, a haze removal algorithm for UAV images based on robust estimation of atmospheric light was proposed. The proposed algorithm selects image patches with diff...

Online fault detection based on dual modular redundancy for embryonics array
LI Danyang, CAI Jinyan, MENG Yafeng, ZHU Sai
2017, 43(6): 1112-1122. doi: 10.13700/j.bh.1001-5965.2016.0745
Abstract:

In order to solve the problems for embryonics array that online fault detection is difficult to be designed, detection rate is low, and detection rate is difficult to be accurately calculated, an online fault detection method based on dual modular redundancy and a fault detection rate analysis metho...

Refined tracking algorithm for steady partly resolvable group targets based on ICP
WANG Cong, WANG Haipeng, HE You, GUO Chen
2017, 43(6): 1123-1131. doi: 10.13700/j.bh.1001-5965.2016.0421
Abstract:

To deal with the problem of the refined tracking of steady groups in partly resolvable condition, a refined tracking algorithm based on iterative closest point (ICP) is proposed in this paper. First, the ICP algorithm is used in tracking association, and by using closest point cyclic iteration, the ...

Fault-tolerant control of UAV anti-skid braking system with input and output constraints
SUN Hui, YAN Jianguo, QU Yaohong
2017, 43(6): 1132-1140. doi: 10.13700/j.bh.1001-5965.2016.0438
Abstract:

In this paper, a method of adaptive neural network backstepping fault-tolerant control, based on barrier Lyapunov function, is proposed for anti-skid braking system in the presence of slip-ratio constraint, control input saturation and partial loss of actuator effectiveness. The neural network can m...

Photovoltaic multi-peak output characteristics and GMPPT control under complex shaded condition
CHEN Mingxuan, WU Jianwen, MA Suliang, HUANG Lian
2017, 43(6): 1141-1148. doi: 10.13700/j.bh.1001-5965.2016.0478
Abstract:

Aimed at solving the failure problem of the maximum power point tracking (MPPT) algorithm caused by partially shaded condition in the photovoltaic power generation system, a global maximum power point tracking (GMPPT) algorithm based on δ-potential well is proposed. Based on the photovoltaic multi-p...

Analysis on process parameters of laser bending of preloaded metal plate
XU Lang, LI Weidong, WANG Xiufeng, WAN Min
2017, 43(6): 1149-1154. doi: 10.13700/j.bh.1001-5965.2016.0494
Abstract:

Laser bending of preloaded metal plate is a relatively new bending method and its process parameters are researched in this paper. A finite element model of the forming process was established based on software ABAQUS, and its reliability was verified by test. Then, finite element simulations using ...

Internet information processing for earthquake emergency response
SONG Jiangong, WANG Zhixin, LI Qinyong, LI Yating, MA Shilong, LYU Jianghua
2017, 43(6): 1155-1164. doi: 10.13700/j.bh.1001-5965.2016.0785
Abstract:

In recent years, the domestic and international earthquake disaster has caused huge losses to human life and property. Massive earthquake disaster information on the Internet can provide the basis for decision support for emergency response and timely rescue, so there is an urgent need for efficient...

Compensation method of in-track coupling effect of cross-track maneuver for formation-flying satellites
WANG Youliang, LI Mingtao, ZHENG Jianhua, ZHOU Jing
2017, 43(6): 1165-1172. doi: 10.13700/j.bh.1001-5965.2016.0437
Abstract:

Tetrahedron formation has an important application in the space physical three-dimensional collaborative detection. Formation keeping control must be carried out to guarantee the detecting efficiency. However, the in-track coupling effect of cross-track maneuver can cause the drift along the in-trac...

Comparative study of thermal-chemical reaction models on simulation of hypervelocity flow
ZHOU Kai, LI Xudong, HU Zongmin, JIANG Zonglin
2017, 43(6): 1173-1181. doi: 10.13700/j.bh.1001-5965.2016.0474
Abstract:

Hypervelocity flow is the high-speed high-temperature flow environment that space vehicles or capsules face when they reenter the atmospheric layer. An expansion tube is one of the few qualified test facilities on the ground to simulate it. Numerical simulation is presented as a powerful assistant t...

Improved ADT searching method in overlapping grid assembly
LI Peng, GAO Zhenxun, JIANG Chongwen, LEE Chunhian
2017, 43(6): 1182-1190. doi: 10.13700/j.bh.1001-5965.2016.0425
Abstract:

An improved searching method of alternating digital tree (ADT) is proposed for making up the deficiency of the existing ADT method and improving the efficiency of the overlapping grid assembly. The new method stores and retrieves donor cells based on a hash data structure, in which an auxiliary Cart...

Momentum equalization control of space robot with control moment gyroscopes for joint actuation
FENG Xiao, JIA Yinghong, XU Shijie
2017, 43(6): 1191-1198. doi: 10.13700/j.bh.1001-5965.2016.0427
Abstract:

An angular momentum equalization control method was proposed for redundant space robot with scissored-pair control moment gyroscopes (CMGs) for joint actuation. This method utilizes the space robot's extra degrees of freedom to equalize momentum usage among arm links, thus achieving CMGs' simultaneo...

An efficient method for reliability global sensitivity index by space-partition
YUN Wanying, LYU Zhenzhou, JIANG Xian, YANG Caiqiong
2017, 43(6): 1199-1207. doi: 10.13700/j.bh.1001-5965.2016.0479
Abstract:

The reliability sensitivity index well analyzes how the failure probability of a model is affected by the different sources of uncertainty in the model inputs. In order to improve the efficiency of digital simulation in estimating this index, a method was proposed based on the weighted density, the ...

Quantitative spectral modeling method based on improved extreme learning machine
ZHOU Meiling, ZHENG Dezhi, LOU Ge, LIU Zheng
2017, 43(6): 1208-1215. doi: 10.13700/j.bh.1001-5965.2016.0459
Abstract:

According to the principle of near infrared spectrum (NIR), an optimized extreme learning machine algorithm with particle swarm optimization (PSO-ELM) was proposed and used in ammonia concentration quantitative analysis of small sample. By optimizing the hidden node parameters of extreme learning ma...

Space position reconstruction of ballistic target based on adaptive fusion
XU Dan, TIAN Bo, FENG Cunqian, HE Sisan, ZHAO Shuang
2017, 43(6): 1216-1223. doi: 10.13700/j.bh.1001-5965.2016.0463
Abstract:

Aimed at the problem that signal radar extracts parameters difficultly and has higher error in estimating parameters due to coupling of precession cone target parameters, a novel algorithm based on uniting the multi-aspect micro-motion information is proposed for parameter extraction and fusion. Fir...

A fast algorithm for long-term fluid-solid conjugate heat transfer process
MENG Fanchao, DONG Sujun, JIANG Hongsheng, WANG Jun
2017, 43(6): 1224-1230. doi: 10.13700/j.bh.1001-5965.2016.0447
Abstract:

Concerning the specific demands for solving problems of the long-term conjugate heat transfer (CHT) problem at the kilosecond level, a new loosely coupled algorithm of the global tightly transient coupled heat transfer based on the quasi-steady flow field is put forward. The flow field is updated al...

Gravity compensation of an intraocular surgery robot based on computed torque method
CHEN Xiang, HUANG Long, YANG Yang
2017, 43(6): 1231-1238. doi: 10.13700/j.bh.1001-5965.2016.0455
Abstract:

To improve the positioning accuracy and stability of an intraocular surgery robot which has a remote center of motion (RCM) mechanism, the coordinate system of the robot is established. Based on the equivalent system model, the instantaneous centroid position of model components is analyzed. The dyn...

Sparse principal component analysis via regularized rank-k matrix approximation
YANG Qian, LIU Hongying
2017, 43(6): 1239-1246. doi: 10.13700/j.bh.1001-5965.2016.0462
Abstract:

In calculating the sparse principal components (PCs), attaining k PCs simultaneously can reduce the accumulated error arising from the calculation process. We proposed the sparse principal component model via regularized rank-k matrix approximation and designed a block coordinate descent method (BCD...

Effect of radar signal error on automatic carrier landing control of carrier-based aircraft
YANG Baojun, LIU Gang, HONG Guanxin
2017, 43(6): 1247-1253. doi: 10.13700/j.bh.1001-5965.2016.0475
Abstract:

The effect of signal error on carrier landing during radar navigation was analyzed based on the automatic carrier landing system (ACLS) of natural carrier-based aircraft and the commissioned main guiding way of radar navigation in carrier landing. According to the components and the functions of the...

Availability evaluation of PBN and ADS-B application for BDS/GPS combined H-ARAIM
GE Yishan, WANG Zhipeng
2017, 43(6): 1254-1263. doi: 10.13700/j.bh.1001-5965.2016.0477
Abstract:

Horizontal-advanced receiver autonomous integrity monitoring (H-ARAIM) is a new type of airborne autonomous satellite navigation integrity monitoring technology developed in the United States and Europe. In view of performance based navigation (PBN) and automatic dependent surveillance-broadcast (AD...

Application of GO-FLOW methodology in reliability analysis of aircraft EHA
LAN Xue, DUAN Fuhai, SANG Yong
2017, 43(6): 1264-1270. doi: 10.13700/j.bh.1001-5965.2016.0444
Abstract:

The GO-FLOW methodology is applied in the reliability analysis of aircraft electro-hydrostatic actuator (EHA). Firstly, based on the reasonable division of unit function, GO-FLOW reliability analysis model of EHA was established. In order to solve the difficult problem that GO-FLOW chart cannot cont...

Simulation and test verification of piezoelectric cantilever vibration energy harvester
SI Jianhang, DAI Yuting, YANG Song, WANG Chaolei, WANG Ruoqin, YANG Chao
2017, 43(6): 1271-1277. doi: 10.13700/j.bh.1001-5965.2016.0416
Abstract:

Piezoelectric ceramic vibration energy harvester has attracted great attention for its simple structure, environment protection, easy miniaturization and other advantages. According to piezoelectric effect, a double-coupled distributed parameter model was established using mode method by combination...

Temperature rise characteristic of lithium battery integrated thermal management system combining phase change materials with air cooling
SHI Shang, YU Jianzu, XIE Yongqi, GAO Hongxia, LI Ming
2017, 43(6): 1278-1286. doi: 10.13700/j.bh.1001-5965.2016.0831
Abstract:

A large amount of heat inside the lithium battery must be dissipated to ensure the safety of the battery by using high efficiency thermal management system (TMS) at high charging/discharging rates. A newly designed TMS integrating phase change material with air cooling was designed and its temperatu...