Results 21 to 30 of about 500,409 (312)
Analysis of the Optimal Frequency Band for a Ballistic Missile Defense Radar System [PDF]
Journal of the Korean Institute of Electromagnetic Engineering and Science, 2018 In this paper, we consider the anti-attack procedure of a ballistic missile defense system (BMDS) at different operating frequencies at its phased-array radar station.
Dang-An Nguyen +4 more
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An optimal nonlinear guidance logic for the trajectory tracking of supercavitating vehicles [PDF]
, 2017 Supercavitating vehicles (SV) are a class of high-speed autonomous underwater vessels. They present a great challenge in designing the guidance law in comparison with the traditional autonomous underwater vehicles.
Gao, Ke, Song, Jia, Yang, Erfu
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Surrogate-Based Optimization Design for Air-Launched Vehicle Using Iterative Terminal Guidance
Aerospace, 2022 In recent years, the penetration of low-cost air-launched vehicles for nano/micro satellites has significantly increased worldwide. Conceptual design and overall parameters optimization of the air-launched vehicle has become an exigent task.
Jiaxin Li, Donghui Wang, Weihua Zhang
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Anti-Saturation and Undecoupled Diving Attack Guidance Law for Impact Angle and Time Constraints [PDF]
Hangkong bingqi, 2023 Aiming at the characteristics of the motion model of the dive attack segment of hypersonic vehicle, such as strong nonlinearity, strong coupling between channels, complex constraints and easy overload saturation under the limit condition, a kind of anti ...
Ge Song, Xia Wenjie, Yan Xunliang
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Impact-Time-Control Guidance Law for Hypersonic Missiles in Terminal Phase
IEEE Access, 2020 Recent researches on hypersonic vehicles adopted in military have gained a lot of interest because of its high flight speed and efficiency. However the guidance laws for hypersonic missiles against the anti-missile system to increase survivability and ...
Chenhao Zhu +4 more
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Aerospace, 2023 Focusing on the large maneuver penetration of the hypersonic glide vehicle with multiple constraints and uncertain disturbance, a robust integrated guidance and control law, which can achieve the snake-shape maneuver, is designed.
Xiaojun Yu, Shibin Luo, Haiqiao Liu
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Impact-Angle-Control Guidance Law with Terminal Constraints on Curvature of Trajectory
Mathematics, 2023 This paper presents an impact-angle-control guidance law with terminal constraints on the curvature of the missile trajectory. The formulation takes into account nonlinear kinematics and time-varying velocity, allowing for more general cases in which the
Kyoung-Rok Song, In-Soo Jeon
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Xibei Gongye Daxue XuebaoIn order to solve the cooperative attack problem during the terminal guidance phase for loitering munition swarm, a cooperative attack strategy for loitering munitions with impact angle constraints is proposed.
ZHAO Junmin +3 more
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Optimal terminal guidance for exoatmospheric interception
Chinese Journal of Aeronautics, 2016 AbstractIn this study, two optimal terminal guidance (OTG) laws, one of which takes into account the final velocity vector constraint, are developed for exoatmospheric interception using optimal control theory. In exoatmospheric interception, because the proposed guidance laws give full consideration to the effect of gravity, they consume much less ...
Yu, Wenbin +4 more
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Linear Gauss Pseudospectral Method Using Neighboring Extremal for Nonlinear Optimal Control Problems
AerospaceThis article proposes a method to solve nonlinear optimal control problems with arbitrary performance indices and terminal constraints, which is based on the neighboring extremal method and Gauss pseudospectral collocation.
Tianyou Zhang, Wanchun Chen, Liang Yang
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