<?xml version="1.0" encoding="utf-8"?>
<rss version="2.0" xmlns:atom="http://www.w3.org/2005/Atom" xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005">
<channel xmlns:cfi="http://www.microsoft.com/schemas/rss/core/2005/internal" cfi:lastdownloaderror="None">
<title cf:type="text"><![CDATA[Editorial department of the Journal of National University of Defense Technology -->控制科学与工程·机械工程·物理学]]></title>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Estimation of towed linear array shape using tug track during ship′s course-change maneuvering]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202004012]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[Aiming at the problem of the limited application scope of water-pulley model, a method for smoothing the tug track to obtain the track of the sonar array and estimate the array shape was proposed. By analyzing the steady-state vibration response characteristics of the array, it is considered that each point on the sonar array moves along the same track. The smoothing window was designed to smooth the tug track into the track of sonar array during circular maneuver, and was extended to the scene of course-change maneuvering. A part of the window was used to smooth the track portion, whose distance from the tug is less than the width of the smooth window, to obtain the current cable shape, so as to estimate the shape of the whole array during the course-change maneuvering. The simulation results show that if the array consists of 81 elements spaced at 5 m, the proposed method can increase the average array gain during course-change maneuvering by about 0.8 dB and lower the average direction estimation error by about 4.7° compared with the original water-pulley model. Using the simulation results to analyze the input sensitivity of the algorithm, the proposed method was simplified to make it easier to implement. Verification using sea trial data shows that the simplified method is feasible and effective.]]></description>
<pubDate>2020/8/8 11:01:28</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[XI Chang, CAI Zhiming, YUAN Jun]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>XI Chang, CAI Zhiming, YUAN Jun</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202004012]]></guid><cfi:id>21</cfi:id><cfi:read>true</cfi:read></item>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Motion parameter estimation of magnetic ship target based on multi-channel convolutional neural network]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202004013]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[In order to overcome this defect of traditional magnetic target motion estimation′s dependence on the initial state information of the target, a three-axis projection model of magnetic moving ship targets was established, and 10 kinds of target training datasets, validation data sets and test data sets of magnetic ship moving targets with variable parameters were generated. Multi-channel convolutional neural network was designed to estimate the distance abeam and velocity of the target, and the effects of different learning methods and activation functions on the performance of the network were compared and analyzed. The results show that the performance of Adam+tanh method is better than other methods, and the estimation effect of motion parameters is accurate. Compared with Kalman filter and particle filter, this estimation algorithm is calculated with preferable efficiency and independent of initialization for estimation.]]></description>
<pubDate>2020/8/8 11:01:28</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[MA Jianfei, YAN Bing, LIN Chunsheng, CHEN Hao]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>MA Jianfei, YAN Bing, LIN Chunsheng, CHEN Hao</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202004013]]></guid><cfi:id>20</cfi:id><cfi:read>true</cfi:read></item>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Numerical modeling for new prevention and control technologies of air wake field of large ships]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202004014]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[Because the air wake fields of large ships have a great influence on the safety of aircraft landing, therefore, the effective technologies to guarantee the safety of aircraft and maritime activities are of great significance. The CFD(computational fluid dynamics) method was used to study the air wake field characteristics of large ships and the prevention and control technologies. The Reynolds averaged Navier-Stokes equations with Spalart-Allmaras turbulence model were used to construct simulation platform, the numerical modeled work was carried out through the platform. The regular and characteristic of air wake fields of large ships were analyzed. Furthermore, the new prevention and control technologies of air wake field of large ships were proposed, and the theoretical basis, center method and technical proposal were expounded. According to the thinking and theory of active blowing prevention and control technology, numerical modeling method was used to test the new prevention and control technologies of air wake field of large ships. Numerical results show that the new method can significantly improve the quality of the air wake field, make the flow field stable and uniform, and hence it can reduce the impacts on the aircraft landing on large ships. After the method is further improved, the engineering application can be realized to ensure the safety of aircraft landing on ships, potentially.]]></description>
<pubDate>2020/8/8 11:01:29</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[SU Shipeng, CAO Xiaoqun, ZHANG Daquan, WEI Zhiyuan]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>SU Shipeng, CAO Xiaoqun, ZHANG Daquan, WEI Zhiyuan</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202004014]]></guid><cfi:id>19</cfi:id><cfi:read>true</cfi:read></item>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Poisoning characteristics of LaB<sub>6</sub> hollow cathode]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202004015]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[Compared with other cathodes, LaB<sub>6</sub> cathode has the advantage of high electron emission current density, and has been widely used in electric propulsion, high emission density electron gun and other products. In order to analyze the poisoning characteristics of the LaB<sub>6</sub> hollow cathode and identify its failure mode, the performance change features and reasons of LaB<sub>6</sub> hollow cathode exposed to atmosphere were studied. The results show that the LaB<sub>6</sub> hollow cathode adsorbs a great deal of poisonous gas on the surface of the emitter during exposure to the atmosphere, and while the work function from the emitter surface increases, the emitter appears short-term poisoning phenomenon. The discharge voltage and hollow cathode plate temperature are increased, and the discharge voltage and cathode top temperature are restored to the initial state after short-term operation. However, if the poisoning phenomenon of LaB<sub>6</sub> hollow cathode is serious, the oxide generated on the surface can not be removed by heating and ion bombardment. Therefore, the emitter state of hollow cathode can be indirectly characterized by monitoring the change of cathode temperature and anode voltage during the test.]]></description>
<pubDate>2020/10/21 15:55:40</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[YANG Wei, ZHANG Tianping, LONG Jianfei, GUO Ning, LIU Mingzheng, GU Zengjie]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>YANG Wei, ZHANG Tianping, LONG Jianfei, GUO Ning, LIU Mingzheng, GU Zengjie</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202004015]]></guid><cfi:id>18</cfi:id><cfi:read>true</cfi:read></item>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Multi-stage sensor-weapon joint task management method]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202004016]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[The sensor-weapon joint task management under dynamic environment was studied. The stage threshold, which determines the beginning of next stage, was set according to the number of valid newly appearing targets, idle sensors and weapons during the dynamic combat process. The multi-stage combat process was constructed. The effect of distributed combat system to the quality of attack scheme and the response time of system was analyzed. As a result the system could decide the response flow of each task management stage independently. The superiority of constructing distributed combat system and setting the stage threshold was verified by simulations.]]></description>
<pubDate>2020/10/21 15:55:40</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[CHEN Chen, XU Wenqin, ZHANG Mingyang]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>CHEN Chen, XU Wenqin, ZHANG Mingyang</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202004016]]></guid><cfi:id>17</cfi:id><cfi:read>true</cfi:read></item>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Evolution law and importance analysis of equipment structure]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202004017]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[Based on the status quo of modularization of equipment design, the evolution of equipment structure and the order of importance ranking by using importance theory were analyzed. On the basis of the gradual evolution from single component to five-component structure and N-component series-parallel structure, the evolution law was sorted out, and the importance analysis of the typical structure was carried out. The evolution of equipment structure and the order of importance of each component are obtained, which fills in the blank of the research on the importance drift law of the equipment, and provides technical support for the reliability optimization design of the equipment.]]></description>
<pubDate>2020/10/21 15:55:40</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[DUI Hongyan, BAI Guanghan, ZHANG Yunan, ZHANG Xiaoke, WANG Chuang]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>DUI Hongyan, BAI Guanghan, ZHANG Yunan, ZHANG Xiaoke, WANG Chuang</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202004017]]></guid><cfi:id>16</cfi:id><cfi:read>true</cfi:read></item>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Improved adaptive Hatch filter algorithm to minimize effects of ionospheric anomaly for GBAS]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202004018]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[Aimed at the problem that the smoothing accuracy of Hatch filter in single frequency GBAS (ground based augmentation system) is reduced by the ionospheric anomaly, the influence of ionospheric delay on the smoothing accuracy of Hatch filter was analyzed systematically, and an improved adaptive Hatch filter algorithm was proposed. The code-carrier divergence was calculated according to the satellite signal, and its high frequency was suppressed by using the second-order linear time-invariant filter to detect whether the ionosphere is abnormal. A function model between the root mean square of smoothed pseudorange error and the ionospheric delay rate, the standard deviation of pseudorange measurement noise and the smoothing time was established, from which the optimal smoothing time of Hatch filter was determined. The verification experiments were carried out by using GBAS prototype developed in the laboratory. The experimental results show that the adaptive Hatch filter algorithm is able to calculate the optimal smoothing time according to the ionospheric delay rate of satellite signal. When the ionospheric is abnormal, the maximum airborne position error is reduced from 1.15 m to 0.43 m, which verifies the effectiveness of the proposed algorithm.]]></description>
<pubDate>2020/10/21 15:55:40</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[HU Jie, ZHU Yixian, SHAN Yao]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>HU Jie, ZHU Yixian, SHAN Yao</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202004018]]></guid><cfi:id>15</cfi:id><cfi:read>true</cfi:read></item>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Application of the improved BAS-TIMS algorithm in air combat maneuver decision]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202004019]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[Owing to the low accuracy and poor real-time ability of modern air combat maneuver decision-making, the BAS-TIMS (beetle antennae search-tactical immune maneuver system) algorithm was improved and applied to air combat maneuver decision-making. The traditional maneuver inventory was enlarged by adding four maneuvers, left climbing, right climbing, left diving, right diving. Eleven basic maneuver tactics were designed, and a method was given to control them. Considering range, height, speed, angle and the superiority function of fighter performance, a comprehensive superiority function of fighter performance was built with the help of nonparametric model. Monte Carlo probability iteration was introduced into the beetle antennae search algorithm to improve its global search ability and convergence speed. This algorithm was combined with TIMS, and the improved BAS-TIMS algorithm was applied into modern air combat maneuver decision-making. An example was given to simulate and prove the effectiveness by comparing BAS-TIMS with game theory, the improved symbiotic immune evolutionary algorithm, the traditional BAS algorithm and the traditional TIMS model. The simulation results show that the improved BAS-TIMS algorithm has more advantages on convergence speed, accuracy and global search ability in air combat maneuver decision-making.]]></description>
<pubDate>2020/10/21 15:55:40</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[JI Huiming, YU Minjian, QIAO Xinhang, YANG Haiyan, ZHANG Shuaiwen]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>JI Huiming, YU Minjian, QIAO Xinhang, YANG Haiyan, ZHANG Shuaiwen</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202004019]]></guid><cfi:id>14</cfi:id><cfi:read>true</cfi:read></item>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[An overview of code-based encryption schemes]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202004020]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[The quantum algorithm which was put forward recently has led to great insecurity of cryptographic analysis of the coding under quantum computing. The future of the code-based cryptography with anti-quantum attack properties was questioned by many people. However, in the research process, people gradually had a deep understanding of the advantages and disadvantages of its encryption scheme. At present, the code-based cryptography has become one of the most promising post-quantum cryptography schemes. The code-based encryption schemes were summarized and the existing attacks of their original schemes were analyzed. Finally, the nature of the security problem of encoding-based encryption system is analyzed, and the future development direction is expounded.]]></description>
<pubDate>2020/10/21 15:55:40</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[LI Zhe, HAN Yiliang, LI Yu, ZHU Shuaishuai, YANG Xiaoyuan]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>LI Zhe, HAN Yiliang, LI Yu, ZHU Shuaishuai, YANG Xiaoyuan</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202004020]]></guid><cfi:id>13</cfi:id><cfi:read>true</cfi:read></item>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Quasi-static compression energy absorption mechanism of filament wound composite constrained spherical buoyancy core material]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202003011]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[In order to meet the demand of the impact protection and the buoyancy reserve of sea structure platform, a new energy absorption structure of filament wound composite constrained spherical buoyancy core material element was designed. The numerical simulation analysis and experimental test verification were carried out for the structure element by using the ABAQUS finite element software and electronic universal material testing machine in order to investigate the damage modes and energy dissipation mechanism. Further analysis of the mechanical response characteristics and damage modes shows that the key to the structural energy absorption design lies in the matching of the Poisson's ratio of the surface layer and the core material. The core material absorbs energy mainly through plastic compression damage and shear fracture damage, while the surface energy absorption is mainly through circular petal-shaped tensile fracture damage. The results show that this type of structural unit has excellent compression and energy absorption characteristics, and can realize the protection energy absorption and buoyancy reserve requirements of the offshore engineering structure platform.]]></description>
<pubDate>2020/7/6 0:00:00</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[ZHOU Xiaosong, ZHANG Yanbing, MEI Zhiyuan]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>ZHOU Xiaosong, ZHANG Yanbing, MEI Zhiyuan</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202003011]]></guid><cfi:id>12</cfi:id><cfi:read>true</cfi:read></item>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[High-temperature failure characteristics of phenolic-quartz hybrid fabrics reinforced benzoxazine composites]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202003012]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[P-Q/BZ(Phenolic-quartz hybrid fabrics reinforced benzoxazine resin composites) were manufactured by compression molding. The flexural properties, ablative properties, resistance to flow erosion and failure characteristics of the P-Q/BZ specimens were investigated. The applicability of P-Q/BZ in high temperature environment was studied. Results showed that, the average flexural strength, flexural modulus and ILSS (interlaminar shear stress) of virginal P-Q/BZ specimens were 283 MPa, 10.8 GPa and 22.6 MPa, respectively. After 300 ℃ thermal treatment in N2 atmospheres:the thickness of P-Q/BZ specimens were increased by about 22%, and the flexural strength, flexural modulus and ILSS of P-Q/BZ specimens were decreased by about 58%, 41% and 58%, respectively. After the oxyacetylene flame test, the average mass loss rate and the linear ablative rate of P-Q/BZ specimens were 0.048 4 g/s and -0.081 mm/s, respectively. No delamination of the P-Q/BZ composites were observed but the microstructure of the char layer delaminated severely, the carbonaceous residue blocks which were produced by the phenolic fiber and the resin matrix were attached badly to the quartz fibers. The resistance to heat-flow erosion of the P-Q/BZ specimen was significantly affected, and the mass loss of the P-Q/BZ composite was about 59% after the exhaust plume ablative test with a small liquid motor. Pyrolysis expansion problem of the P-Q/BZ composites is in need of a solution and the resistance to heat-flow erosion of this composites is in demand of improvement as well.]]></description>
<pubDate>2020/7/6 10:23:21</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[BIAN Liping, XING Suli, YIN Changping]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>BIAN Liping, XING Suli, YIN Changping</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202003012]]></guid><cfi:id>11</cfi:id><cfi:read>true</cfi:read></item>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Smooth switching scheme for the control of CO oxidation reaction rate in hydrogen production]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202003013]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[The catalytic CO oxidation on platinum group metals exhibits complex intrinsic nonlinear properties, such as reaction rate catastrophe, bistability, and hysteresis. These intrinsic nonlinear properties depend on the inherent stability and self-organization mechanism of the chemical reaction. A corresponding phenomenon is a path-dependent input-output relationship between the CO oxidation reaction rate and the control parameters. The traditional linear control method for these systems has an inherently unstable mechanism that can give rise to the oscillation of the chemical reaction rate and the instability of the control system. However, the previous application of ordinary nonlinear switching control faces a large disturbance at the initial moment of switching, which will affect the dynamic performance and stability of the control system. For this reason, a smooth switching control method based on the integral initial value reset was proposed. The results show that the proposed method can provide a smooth switching control of CO oxidation reaction rate, and thus the dynamic performance of the control system is improved.]]></description>
<pubDate>2020/7/6 10:23:21</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[ZHANG Lei, SHENG Li]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>ZHANG Lei, SHENG Li</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202003013]]></guid><cfi:id>10</cfi:id><cfi:read>true</cfi:read></item>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[A comparative study of system schemes for LOX/LCH<sub>4</sub> expander cycle liquid rocket engine]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202003014]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[The researches about the LOX/LCH<sub>4</sub> expander cycle throttling liquid rocket engine are rare and its recognition of it is not distinct, especially at the system level. Based on the whole engine system, the theoretical method was adopted to investigate the work capacity of CH<sub>4</sub> and the feasibility of throttling schemes. The single-turbine and double-turbine throttling schemes were given, and the detailed comparison between them was analyzed. The results reveal that CH<sub>4</sub> work capacity decreases at first and then increases with the decrease of chamber pressure. And the proposed throttling schemes are feasible. Moreover, compared with the single-turbine scheme, the oxidizer and fuel mass flows can be adjusted respectively for double-turbine scheme and the mixture ratio can keep constant better. Meanwhile, the work capacity of CH<sub>4</sub> for double-turbine scheme is much higher, the powers of the oxygen and fuel turbines vary in a narrow range, and the turbines work in a more relaxed environment. Therefore, considering the system reliability, the double-turbine scheme is advantageous to a certain extent.]]></description>
<pubDate>2020/7/6 10:23:21</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[CUI Peng, LI Qinglian, CHENG Peng, ZHANG Beichen]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>CUI Peng, LI Qinglian, CHENG Peng, ZHANG Beichen</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202003014]]></guid><cfi:id>9</cfi:id><cfi:read>true</cfi:read></item>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Adaptive collaborative fault tolerance for multi-agent formation system with hybrid actuator faults and multiple unknown control directions]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202202017]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[The cooperative fault-tolerant for the nonlinear multi-agent system with hybrid actuator faults and multiple unknown control directions were investigated, based on the RAFSMT(robust adaptive fuzzy sliding mode technology). The piecewise Nussbaum function was used to solve the multiple unknown control directions, and the robust adaptive fuzzy technology was used to solve the nonlinear uncertainty in the system. A first-order sliding mode differentiator was introduced, and it was combined with the adaptive backstepping technique to obtain the first-order derivative of the virtual control law. At the same time, a robust bounded method was adopted to improve the convergence speed and tracking accuracy of the designed adaptive cooperative controller. Based on the algebraic graph theory, the error model of the agent system was established, the distributed consensus cooperative fault-tolerant controller was designed, and the Lyapunov candidate function was constructed to prove that the proposed controller can make the system stable. The effectiveness of the proposed method is verified by the comparison of simulation examples, which provides theoretical support for engineering practice.]]></description>
<pubDate>2022/4/1 11:52:58</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[ZHANG Pu, XUE Huifeng, GAO Shan, ZUO Xuan]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>ZHANG Pu, XUE Huifeng, GAO Shan, ZUO Xuan</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202202017]]></guid><cfi:id>8</cfi:id><cfi:read>true</cfi:read></item>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Performance optimization of infrared interference decoy based on trajectory correction technique]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202202018]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[In order to solve the performance optimization problem caused by the high-dimensional nonlinear characteristics of the trajactory correction decoy and improve the traditional serial design method in the conceptual design stage, an intelligent optimization algorithm based on DOE (design of experiments) and RSM (response surface methodology) was proposed and the basic projectile structure model and related design parameters were defined. Based on the DOE, the design variables were mapped to the performance criteria to generate the stochastic Kriging response surface, and the neural network was trained to identify the unstable design. Multi population genetic algorithm was used to determine the optimal projectile design. By changing its cost function, the Pareto frontier reflecting the performance tradeoff could be generated. Simulation results show that as for the technical transformation of infrared interference decoy based on trajectory correction, the proposed algorithm can obtain the optimal design configuration quickly and accurately in the conceptual design stage, which can guarantee the following accompanying flight mission.]]></description>
<pubDate>2022/4/1 11:52:58</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[XING Bingnan, DU Zhonghua, DU Chengxin]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>XING Bingnan, DU Zhonghua, DU Chengxin</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202202018]]></guid><cfi:id>7</cfi:id><cfi:read>true</cfi:read></item>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Structure analysis and design optimization of pneumatic soft manipulator]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202202019]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[The motion and mechanical characteristics of pneumatic soft manipulators are significantly affected by their structural characteristics. At present, it is urgent to improve the support reaction force and inclination angle of the pneumatic soft manipulator. Based on the script interface provided by ABAQUS, Python script was developed to establish a parametric simulation model of gas control software drive, using the size factor as the optimization variable, linking Isight and ABAQUS, and to determine the high sensitivity influence factor of inclination angle and support reaction force by single factor test method.The normalization and weighting strategy and the evolutionary optimization algorithm were used to optimize the inclination angle and the support reaction force, thereby obtaining optimal parameter combination. The results show that the support reaction force and inclination angle are increased by 29% and 136% respectively compared with the initial value of the response. The combination of finite element calculation and multi-variable optimization of the pneumatic soft manipulator is realized and the bending deformation capacity and load capacity of the pneumatic soft manipulator are improved simultaneously.]]></description>
<pubDate>2022/4/1 0:00:00</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[LIU Zhuoqun, ZHANG Xiang, HUANG Yiyong, CHEN Xiaoqian, ZHAO Yong]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>LIU Zhuoqun, ZHANG Xiang, HUANG Yiyong, CHEN Xiaoqian, ZHAO Yong</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202202019]]></guid><cfi:id>6</cfi:id><cfi:read>true</cfi:read></item>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Effect of tip winglet on the leakage flow of compressor cascade at high subsonic speed]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202202020]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[To explore effects of different installation locations and different widths of tip winglets on the aerodynamic characteristics of compressor cascades under the condition of transonic incoming flow, the flow fields of seven diffused cascades including the prototype cascade were numerically studied at Ma=0.8. The results show that under the combined influence of various factors, the suction surface tip winglets with different incoming flow attack angles have negative effects in the flow field, and increase the complexity of the flow field. Meanwhile, the pressure surface tip winglets improve the leakage flow and reduce the flow loss. The effect of the tip winglet on the flow field is proportional to its width in both installation positions. The interference or improvement effect of the tip winglet on the flow field is more obvious at positive angle of incidence. Compared with the normal condition, the most obvious effects of the two types of tip winglets can be obtained under the condition of positive 6°. The suction surface tip winglet with a width of 2.0 times of the original width causes 4.17% flow field loss, while the pressure surface tip winglet whose width is 2.0 times of the original width is accompanied by an improvement effect of 10.15%.]]></description>
<pubDate>2022/4/1 11:52:58</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[WU Wanyang, ZHONG Jingjun]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>WU Wanyang, ZHONG Jingjun</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202202020]]></guid><cfi:id>5</cfi:id><cfi:read>true</cfi:read></item>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Modeling and simulation analysis of ultra high pressure common rail system for adjustable fuel injection rate]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202202021]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[Aiming at the problems of low fuel injection pressure and inability to flexibly change the fuel injection rate in the injection process of conventional high pressure common rail system, an ultra high pressure common rail system for adjustable fuel injection rate based on domestic processing capacity and technology was proposed and designed. On the basis of introducing the working principle of this system, the simulation model of system was established via AMEsim software, the accuracy of this model was verified by experiment, and the pressure characteristics and fuel injection control characteristics of the system were studied through the model. A at the same time, the influence of the key structural parameters of the electric-controlled pressure amplifier on the system performance were analyzed. Results show that the ultra high pressure common rail system for adjustable fuel injection rate can magnify fuel pressure to the ultra high pressure state, and by changing the control signal working time of electric-controlled pressure amplifier and injector solenoid valve in system, the flexible and controllable fuel injection rate curve shape can be achieved. Compared with the control chamber volume and spool mass, the fuel outlet diameter and spool displacement have greater influence on the performance of this system, with the increase of fuel outlet diameter and spool displacement, the pressurization pressure and fuel injection rate peak value both increase, while the fuel leakage rate increases first and then decreases.]]></description>
<pubDate>2022/4/1 11:52:58</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[ZHOU Lei, YANG Kun, NIE Tao, WU Xin, LIU Nan]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>ZHOU Lei, YANG Kun, NIE Tao, WU Xin, LIU Nan</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202202021]]></guid><cfi:id>4</cfi:id><cfi:read>true</cfi:read></item>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Critical initiation condition of cylindrical covered charge by double spherical fragments impact]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202202022]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[In order to investigate the shock initiation of missile warhead (cylindrical covered charge) by multiple fragments impact under actual combat conditions, based on Jacobs-Roslund formula of single fragment initiation plane covered charge, the engineering calculation model of the impact critical initiation condition of cylindrical covered charge with single or double spherical fragments were established. The calculation model includes several parameters, such as fragment diameter, impact angle, charge radius and shell thickness. The calculation model results were in good agreement with the simulation results and experimental results, which proves that the calculation model can provide a better prediction of the impact critical initiation condition of cylindrical covered charge with single or double spherical fragments.]]></description>
<pubDate>2022/4/1 11:52:58</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[GUO Chun, GUO Shangsheng, QIAN Jianping, GU Wenbin]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>GUO Chun, GUO Shangsheng, QIAN Jianping, GU Wenbin</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202202022]]></guid><cfi:id>3</cfi:id><cfi:read>true</cfi:read></item>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[On-line measurement test of pressure wavespeed in hydraulic system with high precision]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202202023]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[The pressure wavespeed of pipe flow is the basic physical parameter to analyze and study the stability and dynamic quality of hydraulic system. The three-sensor measurement theory was deduced based on the wave equation of the transmission pipeline, the Foster equivalent shear coefficient model was introduced for high-precision estimation of various influence factors in the hydraulic line, and the Newton-Raphson iterative method was adopted to reduce the data processing error and accurately calculate the pressure wavespeed. An on-line test platform for measuring pressure wavespeed of hydraulic pipeline was built based on theoretical derivation, realizing accurate measurement and calculation of pressure wavespeed of hydraulic system under various working conditions by MATLAB software programming. The test results show that: when the system is under the typical working pressure of 20 bar,50 bar,75 bar and 100 bar, the pressure wavespeed is about 1 320 m/s, 1 338 m/s, 1 363 m/s, 1 380 m/s respectively, and the measurement error is within ±1% in the wave speed interval with a confidence level of 95%; the pressure wavespeed of pipeline increases with the rise of the working pressure, and the function relationship between the two variables was given according to the test results; the effect of pipe material on system flexibility should be considered in the precise calculation of pressure wavespeed. The results of test and analysis have important guiding significance and reference value for the on-line measurement and estimation of pressure wavespeed in hydraulic system.]]></description>
<pubDate>2022/4/1 0:00:00</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[LIANG Yundong, HE Lin, XU Rongwu, CHEN Zongbin]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>LIANG Yundong, HE Lin, XU Rongwu, CHEN Zongbin</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202202023]]></guid><cfi:id>2</cfi:id><cfi:read>true</cfi:read></item>
<item>
<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Theoretical solution of high-order shear deformation beam theory for bending behavior of cylindrical tube on elastic foundation]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202202024]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[The transverse bending of cylindrical tubes embedded in Winkler elastic foundation was studied based on the higher-order shear deformation beam theory. A governing equation for bending of circular cylindrical tubes on elastic foundation or in a surrounding Winkler matrix was derived and accurate solutions were presented for four typical boundary conditions. The obtained results show that the shear stress τ<sub>xr</sub> automatically vanishes on the inner and outer surface of cylindrical tubes when an appropriate warping shape function instead of the shear correction coefficient is chosen. And it can provide analytical solutions with sufficient accuracy for the bending problems of cylindrical tubes with different length-diameter ratios and thickness-diameter ratios. When the stiffness coefficient approaches zero, the deflection curve of cylindrical tube embedded in Winkler elastic foundation approaches the deflection curve of cylindrical tube placed in free space, which verifies the accuracy of the present method. Different from the Euler-Bernoulli beam theory, the normal stress over the cross-section is no longer linear with the abscissa from the neutral surface in this method, and it is especially obvious when the length-diameter ratio is small and the thickness-diameter ratio is large.The shear stress τ<sub>xz</sub> decreases when the distance from the neutral surface becomes large, approaching zero at the top and bottom positions, and the maximum shear stress occurs at the neutral surface which is close to the inner surface.]]></description>
<pubDate>2022/4/1 11:52:58</pubDate>
<category><![CDATA[控制科学与工程·机械工程·物理学]]></category>
<author><![CDATA[MA Weili, SHEN Liulei, SONG Dianyi, LI Xianfang]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>MA Weili, SHEN Liulei, SONG Dianyi, LI Xianfang</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202202024]]></guid><cfi:id>1</cfi:id><cfi:read>true</cfi:read></item>
</channel>
</rss>