云南高校图书馆联盟文献共享服务平台- MISSILE

MISSILE: 作品数：179被引量：483H指数：12; 导出分析报告; 相关领域：兵器科学与技术更多>>; 相关作者：张天桥宋建梅王江华谷良贤龚春林更多>>; 相关机构：北京理工大学北京航空航天大学西北工业大学中国航天科工集团公司更多>>; 相关期刊：更多>>; 相关基金：国家自然科学基金中国航空科学基金中国博士后科学基金航天支撑技术基金更多>>

Closed-form guidance law for velocity maximization with impact angle constraint: 《Journal of Systems Engineering and Electronics》2024年第5期1295-1303,共9页ZHANG Jiahui WEN Qiuqiu; Final velocity and impact angle are critical to missile guidance.Computationally efficient guidance law with compre-hensive consideration of the two performance merits is challeng-ing yet remains less addressed.Theref...; 关键词：MISSILE guidance law proportional-navigation guidance impact angle

Missile guidance law design based on free-time convergent error dynamics: 《Journal of Systems Engineering and Electronics》2024年第5期1315-1325,共11页LIU Yuanhe XIE Nianhao LI Kebo LIANG Yan’gang; supported by the National Natural Science Foundation of China(12002370).; To solve the finite-time error-tracking problem in mis-sile guidance,this paper presents a unified design approach through error dynamics and free-time convergence theory.The proposed approach is initiated by establis...; 关键词：guidance design free-time convergence error dynamics approach impact angle constraint impact time constraint

Time-series satellite remote sensing reveals gradually increasing war damage in the Gaza Strip: 《National Science Review》2024年第9期175-185,共11页Shimaa Holail Tamer Saleh Xiongwu Xiao Jing Xiao Gui-Song Xia Zhenfeng Shao Mi Wang Jianya Gong Deren Li; supported by the National Key Research and Development Program of China(2023YFB3906102);the National Natural Science Foundation of China(42101449,42090012,61825103,U22B2011 and 62325111);the Natural Science Foundation of Hubei Province,China(2022CFB773 and 2020CFA001);the Key Research and Development Program of Hubei Province,China(2022BAA048);the Chutian Scholar Program of Hubei Province and the Yellow Crane Talent Scheme.; War-related urban destruction is a significant global concern,impacting national security,social stability,people’s survival and economic development.The effects of urban geomorphology and complex geological contexts...; 关键词：war damage monitoring satellite remote sensing missile crater detection type of damaged bui lding bui lding damage level detection Gaza Strip

The influence of roll angles on unsteady aerodynamics in a canard-configured missile: 《International Journal of Mechanical System Dynamics》2024年第2期213-225,共13页Kai Wei Shaosong Chen Dongdong Tang Yihang Xu Xujian Lyu Qing Chen; Fund of Science and Technology on Underwater Information and Control Laboratory,Grant/Award Number:2021-JCJQ-LB-030-05。; During the initial stage of vertical launch,a missile may exhibit an uncertain roll angle(φ)and a high angle of attack(α).This study focuses on examining the impact of roll angle variations on the flow field and the...; 关键词：large angle of attack roll angle unsteady separated flow power spectral density proper orthogonal decomposition

Time-varying parameters estimation with adaptive neural network EKF for missile-dual control system: 《Journal of Systems Engineering and Electronics》2024年第2期451-462,共12页YUAN Yuqi ZHOU Di LI Junlong LOU Chaofei; In this paper, a filtering method is presented to estimate time-varying parameters of a missile dual control system with tail fins and reaction jets as control variables. In this method, the long-short-term memory(LST...; 关键词：long-short-term memory(LSTM)neural network extended Kalman filter(EKF) rolling training time-varying parameters estimation missile dual control system

Design methodology of a mini-missile considering flight performance and guidance precision: 《Journal of Systems Engineering and Electronics》2024年第1期195-210,共16页ZHANG Licong GONG Chunlin SU Hua ANDREA Da Ronch; The design of mini-missiles(MMs)presents several novel challenges.The stringent mission requirement to reach a target with a certain precision imposes a high guidance precision.The miniaturization of the size of MMs m...; 关键词：mini-missiles(MMs) GUIDANCE NAVIGATION and control(GNC)system multi-objective optimization multidisciplinary design optimization(MDO) flight performance guidance precision

Quaternion-Based Adaptive Trajectory Tracking Control of a Rotor-Missile with Unknown Parameters Identification: 《Defence Technology（防务技术）》2024年第1期375-386,共12页Jie Zhao Zhongjiao Shi Yuchen Wang Wei Wang; partially supported by the Natural Science Foundation of China (Grant Nos.62103052,52272358);partially supported by the Beijing Institute of Technology Research Fund Program for Young Scholars。; This paper investigates the adaptive trajectory tracking control problem and the unknown parameter identification problem of a class of rotor-missiles with parametric system uncertainties.First,considering the uncerta...; 关键词：Rotor-missile Adaptive control Parameter identification Quaternion control

Uncertainty entropy-based exploratory evaluation method and its applications on missile effectiveness evaluation被引量：2: 《Journal of Systems Engineering and Electronics》2023年第6期1602-1613,共12页HU Jianwen WANG Zhihui GAO Yuan ZHU Xiaomin TIAN Yongliang LIU Hu; the National Natural Science Foundation of China(61872378).; Some attributes are uncertain for evaluation work because of incomplete or limited information and knowledge.It leads to uncertainty in evaluation results.To that end,an evaluation method,uncertainty entropy-based exp...; 关键词：uncertainty entropy-based exploratory evaluation(UEEE) evaluation activity belief degree distribution missile effectiveness.

Improved Fixed-Time Convergence Guidance Scheme Design and Its Application to Missile: 《Guidance, Navigation and Control》2023年第4期85-110,共26页Lei Cui Kang Zhang Xijing Hu Zhe Li Jianying Yang Nan Jin; supported by the National Natural Science Foundation of China under Grant nos.62273250,62073002;the Natural Science Foundation of Tianjin City under Grant no.21JCYBJC00590.; This study presents a fixed-time convergence guidance scheme for impact time and angle control.First,two improved fixed-time stable systems are presented,which have smaller initial control command and better terminal ...; 关键词：Fixed-time stable sliding mode control extended state observer guidance scheme impact time and angle control

Surrogate-assisted optimization for anti-ship missile body configuration considering high-velocity water touching被引量：2: 《Chinese Journal of Aeronautics》2023年第12期268-281,共14页Nianhui YE Teng LONG Junhui MENG Renhe SHI Baoshou ZHANG; co-supported by the National Natural Science Foundation of China(Nos.52272360,52005288,52232014);the Beijing Municipal Natural Science Foundation,China(No.3222019);the BIT Research and Innovation Promoting Project,China(No.2022YCXZ017)。; As a crucial weapon in the sea battle,anti-ship missiles generally employ a sea-skimming penetration strategy to reduce the probability of being detected by the target radar,which greatly increases the risk of touchin...; 关键词：Surrogate-assisted optimiza-tion Fluid-structureinteraction Arbitrary Lagrange-Eulerian MISSILE Conceptual design

高级检索 检索式检索

时间限定

期刊范围

学科限定全选

高级检索 检索式检索

时间限定

期刊范围

学科限定全选

MISSILE

检索结果分析

下载全文

高级检索检索式检索

时间限定

期刊范围

学科限定全选

高级检索 检索式检索

时间限定

期刊范围

学科限定全选

MISSILE

检索结果分析

下载全文

用户登录

高级检索检索式检索