Výsledky vyhľadávania - "MIDCOURSE GUIDANCE"

Trajectory prediction-based guidance law Autor Li, Mengxuan, Guo, Jianguo, Jiang, Ruimin

“…This paper proposes a guidance law based on trajectory prediction, aiming to address the difficulty of traditional guidance laws in meeting high-speed and…”
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Midcourse Guidance for Exoatmospheric Interception Using Response Surface Based Trajectory Shaping Autor Ann, Sungjun, Lee, Seokwon, Kim, Youdan, Ahn, Jaemyung

“…An exoatmospheric midcourse guidance law is proposed to intercept a ballistic missile during the free-flight phase. The proposed guidance law generates a…”
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Active-set pseudospectral model predictive static programming for midcourse guidance Autor Zhou, Cong, He, Lei, Yan, Xiaodong, Meng, Fanqin, Li, Chaoyong

“…This paper focuses on the midcourse guidance law for the interceptor to engage the hypersonic gliding vehicles (HGVs). Firstly, an active-set pseudospectral…”
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Optimal midcourse guidance law for the exo-atmospheric interceptor with solid-propellant booster Autor Zhao, Shilei, Chen, Wanchun, Yang, Liang, Wang, Minghao

“…This paper focuses on the midcourse guidance law for the exo-atmospheric interceptor with solid-propellant booster to intercept a target in the Keplerian…”
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Online midcourse guidance method for boost phase interception via adaptive convex programming Autor Yang, Biao, Jing, Wuxing, Gao, Changsheng

“…This paper proposes an online midcourse guidance method for boost phase interception. Dynamic models are established and flight constraints are analyzed…”
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Disturbance observer-based saturated optimal super-twisting integral sliding mode midcourse guidance against maneuvering targets Autor Chen, Wenxue, Gao, Jiawei, Gao, Changsheng

“…This work addresses the problem of calculating midcourse guidance command in ballistic missile defense techniques against a maneuvering target. An improved…”
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Receding-Horizon Midcourse Guidance for Variable-Flow Ducted Rocket Missiles Autor Kim, Boseok, Jang, Jae-Il, Lee, Heunjae, Lee, Chang-Hun

“…This paper presents an optimization-based midcourse guidance methodology for variable-flow ducted rocket (VFDR) missiles. While classical trajectory…”
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Noniterative feedback midcourse guidance for exo-atmospheric interception of ballistic targets using virtual impact point steering Autor Jo, Byeong-Un, Ahn, Jaemyung

“…This paper proposes a noniterative feedback midcourse guidance algorithm for intercepting a ballistic target. The virtual impact point (VIP) concept, which is…”
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Nonlinear Optimal Midcourse Guidance Using Sequential Pseudospectral Model Predictive Control Autor Xu, Xiang, Chen, Wanchun, Yang, Liang

“…A sequential pseudospectral model predictive control (SPMPC) method is proposed for nonlinear optimal midcourse guidance with a general performance index…”
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A Pseudospectral Model Predictive Solution to Midcourse Guidance for Multistage Interceptor Autor Zhou, Cong, Chen, Sai, Qiao, Hao, Li, Chaoyong, Yan, Xiaodong

“…This article presents an enhanced pseudospectral model predictive static programming (MPSP) approach to address the midcourse guidance problem for an…”
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Group cooperative midcourse guidance law based on multi-layer architecture for intercepting maneuvering target Autor Zhang, Ruitao, Guo, Hang, Chen, Zhan, Fang, Yangwang, Fu, Wenxing

“…To address the actual demand for multi-missile cooperative interception of multi-maneuvering targets, based on the differences in the multi-missile…”
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Pseudo-Spectral MPSP-Based Unified Midcourse and Terminal Guidance for Reentry Targets Autor Sharma, Prayag, Kumar, Prem, Padhi, Radhakant

“…A unified optimal guidance scheme is presented in this article for both midcourse and terminal phases combined. It minimizes the total deceleration resulting…”
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Integrated Target Assignment and Trajectory Optimization for Many-to-Many Midcourse Guidance Autor Jin, Tianyu, Shin, Hyo-Sang, Tsourdos, Antonios, He, Shaoming

“…This article investigates the problem of target assignment and trajectory optimization in multimissile multitarget engagement scenarios. To avoid complex…”
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Multistage Linear Gauss Pseudospectral Method for Piecewise Continuous Nonlinear Optimal Control Problems Autor Li, Yang, Chen, Wanchun, Yang, Liang

“…This article aims at proposing a multistage linear Gauss pseudospectral method (MS-LGPM) for solving the piecewise continuous nonlinear optimal control problem…”
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基于序列凸规划的拦截弹中制导轨迹优化 Autor 李炯, 张锦林, 邵雷, 李万礼, 贺杨超

“…TJ765; 针对强非线性多约束条件下拦截弹中制导轨迹优化问题,基于序列凸规划方法和捕获区域,提出一种针对固定时间约束下的轨迹优化算法.序列凸优化方法求解复杂多项式具有…”
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A Midcourse Guidance Method Combined with Trajectory Prediction for Antinear-Space-Gliding Vehicles Autor Wan, JiaQing, Zhang, Qian, Zhang, Hao, Liu, JiaNing

“…Near-space-gliding vehicles have variable maneuver modes and dramatic changes in their ballistic parameters, which lead to a need to accurately predict an…”
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Midcourse Guidance Trajectory Optimization of Interceptor Missile Based on Sequential Convex Programming Autor Li Jiong, Zhang Jinlin, Shao Lei, Li Wanli, He Yangchao

“…Aiming at the trajectory optimization problem of interceptor midcourse guidance under strong nonlinear multi-constraint conditions, a trajectory optimization…”
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Midcourse phase guidance of an interceptor: a simplified suboptimal onboard implementation technique Autor Sankar, Ram B, Tiwari, Pawan Kishore, Annam, Chandrakanth, Bandyopadhyay, Bijnan, Arya, Hemendra

“…This study deals with the midcourse guidance of an interceptor against various highly maneuvering aerial targets. The interceptors of this class generally use…”
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Trajectory Control of Midcourse Guidance for Air-to-Air Missile Based on Feedback Linearization and Sliding Mode Control Autor Zhang, Chencheng, Tong, Zhiqiang, Liu, Hongquan, Pang, Weijian

“…To guarantee the accuracy and energy efficiency of long-distance midcourse guidance for air-to-air missile, a robust trajectory control method based on…”
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A New Midcourse Guidance Design for Near Space Target Interceptor Autor Wu, Yanrui, Xiao, Mingqing, Zhang, Danxu, Peng, Weishi, Xu, Yang, Dong, Xinyu

“…This study proposes a new midcourse guidance method, combining the trajectory optimization approach and the optimal sliding mode method, to decrease the larger…”
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