Výsledky vyhľadávania - GUIDED MISSILE TRAJECTORIES

Stability of Spinning Missiles Guided by Trajectory Tracking Guidance Law Autor Zhou, Zhiming, Liu, Zhen

“…Trajectory tracking guidance is employed widely by low cost missiles for the characteristic of easy to implement…”
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Terminal attack trajectories of peregrine falcons are described by the proportional navigation guidance law of missiles Autor Brighton, Caroline H, Thomas, Adrian L R, Taylor, Graham K

“… Previous research has looked for simple geometric rules describing the attack trajectories of animals, but the underlying feedback laws have remained obscure…”
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Dynamic optimization of guided missile trajectory by use of Matlab and Dynopt Toolbox Autor Ozana, S., Pies, M., Wagner, P.

“… Particularly it focuses on problem with free time and free end point represented by example of guided missile control in two alternatives…”
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Optimization of the trajectory of the antiaircraft guided missile Autor Izhko, V. A., Yemelyanova, I. A., Reznik, I. M., Khorolskiy, P. G.

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26 Branch Unit No. 96901 Troops of PLA Submits Patent Application for Radar Scene Matching Terminal Guided Missile Flight Trajectory Planning Method

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Scanning program of image guided missile basing on parabolic trajectory Autor Wang Yandong

“…In order to have a larger scanning area of image guided missile which fight baseing on parabolic trajectory, improve the probability of capture by the seeker, a program is presented in the paper…”
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Field-of-View Constrained Three-Dimensional Impact Angle Control Guidance for Speed-Varying Missiles Autor Wang, Jianan, Ding, Xiangjun, Chen, Yadong, Wang, Chunyan, Xin, Ming

“… Furthermore, the trajectory of a guided missile is not affected by the variation of missile speed even under the FOV constraint, which reveals that the impact angle control performance is independent of time-varying missile speed. Numerical simulations are conducted to demonstrate the effectiveness of the proposed guidance law…”
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MISSILE POSITION ESTIMATION USING UNSCENTED KALMAN FILTER Autor Herlambang, Teguh, Subchan, Subchan

“… Therefore, trajectory estimation for guided missiles is the basic requirement…”
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Design and Implementation of Trajectory Planning Algorithm for UAV Borne Air-to-Surface Missile Autor Yang, Kai, Xu, Chen, Xu, Yan

“… missiles for unmanned aerial vehicles. Secondly, it introduces the traditional single-mode guided unmanned aerial vehicle air-to-ground missile trajectory design schemes and the new trajectory planning schemes for multi-mode compound…”
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Penetration trajectory planning based on radar tracking features for UAV Autor Chen, Shaofei, Liu, Hongfu, Chen, Jing, Shen, Lincheng

“…) in the presence of radar-guided surface to air missiles (SAMs).Design methodology approach - The penetration trajectory planning problem is modelled based on four aspects of radar tracking features…”
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Determination of a pitch control program for a solid-propellant missile Autor Siutkina-Doronina, S.V.

“…This paper analyzes the trends in the improvement of the performance characteristics of guided missiles with solid-propellant sustainer engines and identifies the features and requirements for flight…”
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Hybrid Point-Group Target Tracking Using Angle-Only Measurements with Decoy Flares Autor Guo, Xiaoxiao, Lan, Jian, Xi, Ruiqing

“… This becomes more serious when tracking with angle-only measurements provided by the infrared-guided missile, because the target trajectory is hard to estimate accurately…”
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Multi-missile Coordination High Precision Guidance and Control Method for Beam-riding Guidance Autor Guodong, Qi, Jianqiao, Yu, Xiaolin, Ai, Jun, Jiang

“…: through sharing error information between multiple missiles in the same guiding beam, correcting the center line of guided beam and eliminating the steady-state error in the process of missile…”
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Trajectory prediction method for incoming guided projectiles based on the fusion of Temporal Convolutional Network and dual attention mechanisms Autor Gao, Zhanpeng, Yi, Wenjun

“…To improve the response speed and missile interception accuracy of combat systems, this paper proposes a trajectory prediction method for incoming projectiles based on the TCN-ECA-BiGRU-Attention model…”
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Cooperative Guidance for Maneuvering Penetration with Attack Time Consensus and Bounded Input Autor Bin, Zhao, Tianze, Liu, Tianyang, Xiang, Changshu, Wei

“… Firstly, the concept of line deviation control is established, based on which the missile’s maneuvering penetration trajectory is decomposed into a virtual guided trajectory and a relative maneuvering trajectory…”
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Strapdown inertial navigation system based on micromechanical sensors as a part of tank guided missiles Autor N. Borisov, Nikolay, Yu. Solodukhin, Mikhail, I. Godunov, Anatoly

“…Backgroud. The implementation of automatic target capture on the trajectory and the subsequent transition to homing in tank guided missiles is one of the most urgent tasks aimed at increasing the range…”
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Online Trajectory Replan for Gliding Vehicle Considering Terminal Velocity Constraint Autor Kim, Youngil, Cho, Namhoon, Park, Jongho, Kim, Youdan

“…Controlling the terminal velocity can improve the effectiveness of guided missiles…”
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Missile Guidance Design Using Sliding Curve Method Autor Wihardi, Leonard, Kadir, Rusdhianto Effendi Abdul, Hidayat, Zulkifli

“… In this method, the missile is guided according to a pre-determined trajectory by giving reference orientation angles to the missile autopilot system…”
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Thorough Understanding and 3D Super-Resolution Imaging for Forward-Looking Missile-Borne SAR via a Maneuvering Trajectory Autor Gu, Tong, Guo, Yifan, Zhao, Chen, Zhang, Jian, Zhang, Tao, Liao, Guisheng

“…For missile-borne platforms, traditional SAR technology consistently encounters two significant shortcomings…”
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Research on State Estimation Method Applied to Trajectory Prediction of Air Platforms Active Defense Operations Autor Lü Mingyuan, Wu Zhen, Qiao Yaobin

“… It simulates the process of the attack missile guided with proportional guidance law attacking aircraft based on simulation software, to establish an observation model under conditions of constant…”
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