Suchergebnisse - GUIDED MISSILE TRAJECTORIES

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

    ISSN: 1948-9447
    Veröffentlicht: IEEE 15.08.2022
    Veröffentlicht in Chinese Control and Decision Conference (15.08.2022)
    “… Trajectory tracking guidance is employed widely by low cost missiles for the characteristic of easy to implement …”
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    Tagungsbericht
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    Terminal attack trajectories of peregrine falcons are described by the proportional navigation guidance law of missiles von Brighton, Caroline H, Thomas, Adrian L R, Taylor, Graham K

    ISSN: 1091-6490, 1091-6490
    Veröffentlicht: United States 19.12.2017
    “… Previous research has looked for simple geometric rules describing the attack trajectories of animals, but the underlying feedback laws have remained obscure …”
    Weitere Angaben
    Journal Article
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    Dynamic optimization of guided missile trajectory by use of Matlab and Dynopt Toolbox von Ozana, S., Pies, M., Wagner, P.

    ISBN: 9781467322478, 1467322474
    Veröffentlicht: IEEE 01.10.2012
    “… 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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    Tagungsbericht
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    Scanning program of image guided missile basing on parabolic trajectory von Wang Yandong

    ISBN: 1424488095, 9781424488094
    Veröffentlicht: IEEE 01.01.2011
    “… 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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    Tagungsbericht
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    Field-of-View Constrained Three-Dimensional Impact Angle Control Guidance for Speed-Varying Missiles von Wang, Jianan, Ding, Xiangjun, Chen, Yadong, Wang, Chunyan, Xin, Ming

    ISSN: 0018-9251, 1557-9603
    Veröffentlicht: New York IEEE 01.10.2022
    “… 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 …”
    Volltext
    Journal Article
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    MISSILE POSITION ESTIMATION USING UNSCENTED KALMAN FILTER von Herlambang, Teguh, Subchan, Subchan

    ISSN: 1978-7227, 2615-3017
    Veröffentlicht: Universitas Pattimura 01.03.2022
    Veröffentlicht in BAREKENG: Jurnal Ilmu Matematika dan Terapan (01.03.2022)
    “… Therefore, trajectory estimation for guided missiles is the basic requirement …”
    Volltext
    Journal Article
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    Design and Implementation of Trajectory Planning Algorithm for UAV Borne Air-to-Surface Missile von Yang, Kai, Xu, Chen, Xu, Yan

    ISSN: 1742-6588, 1742-6596
    Veröffentlicht: IOP Publishing 01.01.2021
    Veröffentlicht in Journal of physics. Conference series (01.01.2021)
    “… 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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    Journal Article
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    Penetration trajectory planning based on radar tracking features for UAV von Chen, Shaofei, Liu, Hongfu, Chen, Jing, Shen, Lincheng

    ISSN: 1748-8842, 0002-2667, 1758-4213
    Veröffentlicht: Bradford Emerald Group Publishing Limited 01.01.2013
    Veröffentlicht in Aircraft Engineering (01.01.2013)
    “… ) 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 …”
    Volltext
    Journal Article
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    Determination of a pitch control program for a solid-propellant missile von Siutkina-Doronina, S.V.

    ISSN: 1561-9184, 2616-6380
    Veröffentlicht: 19.10.2023
    Veröffentlicht in Technical mechanics (19.10.2023)
    “… 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 …”
    Volltext
    Journal Article
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    Hybrid Point-Group Target Tracking Using Angle-Only Measurements with Decoy Flares von Guo, Xiaoxiao, Lan, Jian, Xi, Ruiqing

    ISSN: 0018-9251, 1557-9603
    Veröffentlicht: IEEE 2025
    “… 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 …”
    Volltext
    Journal Article
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    Multi-missile Coordination High Precision Guidance and Control Method for Beam-riding Guidance von Guodong, Qi, Jianqiao, Yu, Xiaolin, Ai, Jun, Jiang

    ISSN: 1742-6588, 1742-6596
    Veröffentlicht: Bristol IOP Publishing 01.05.2019
    Veröffentlicht in Journal of physics. Conference series (01.05.2019)
    “… : 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 …”
    Volltext
    Journal Article
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    Trajectory prediction method for incoming guided projectiles based on the fusion of Temporal Convolutional Network and dual attention mechanisms von Gao, Zhanpeng, Yi, Wenjun

    ISSN: 0263-2241
    Veröffentlicht: Elsevier Ltd 15.01.2026
    “… 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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    Journal Article
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    Cooperative Guidance for Maneuvering Penetration with Attack Time Consensus and Bounded Input von Bin, Zhao, Tianze, Liu, Tianyang, Xiang, Changshu, Wei

    ISSN: 2093-274X, 2093-2480
    Veröffentlicht: Seoul The Korean Society for Aeronautical & Space Sciences (KSAS) 01.10.2024
    “… 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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    Journal Article
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    Strapdown inertial navigation system based on micromechanical sensors as a part of tank guided missiles von N. Borisov, Nikolay, Yu. Solodukhin, Mikhail, I. Godunov, Anatoly

    ISSN: 2072-3059
    Veröffentlicht: Penza State University Publishing House 01.11.2024
    “… 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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    Journal Article
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    Online Trajectory Replan for Gliding Vehicle Considering Terminal Velocity Constraint von Kim, Youngil, Cho, Namhoon, Park, Jongho, Kim, Youdan

    ISSN: 0018-9251, 1557-9603
    Veröffentlicht: New York IEEE 01.04.2023
    “… Controlling the terminal velocity can improve the effectiveness of guided missiles …”
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    Journal Article
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    Missile Guidance Design Using Sliding Curve Method von Wihardi, Leonard, Kadir, Rusdhianto Effendi Abdul, Hidayat, Zulkifli

    Veröffentlicht: IEEE 01.11.2019
    “… 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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    Tagungsbericht
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    Thorough Understanding and 3D Super-Resolution Imaging for Forward-Looking Missile-Borne SAR via a Maneuvering Trajectory von Gu, Tong, Guo, Yifan, Zhao, Chen, Zhang, Jian, Zhang, Tao, Liao, Guisheng

    ISSN: 2072-4292, 2072-4292
    Veröffentlicht: Basel MDPI AG 01.09.2024
    Veröffentlicht in Remote sensing (Basel, Switzerland) (01.09.2024)
    “… 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 von Lü Mingyuan, Wu Zhen, Qiao Yaobin

    ISSN: 1673-5048
    Veröffentlicht: Editorial Office of Aero Weaponry 01.08.2024
    Veröffentlicht in Hangkong Bingqi (01.08.2024)
    “… 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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    Journal Article