Three-Dimensional Variable Structure Guidance Law for Homing Missile with Terminal Angle Constraints
Proceedings of the 2013 2nd International Conference on Intelligent System and Applied Material, 2011Using the virtual displacement of missile in short time, established a 3-dimensional variable structure guidance (VSG) logic with terminal angle constraints for un-powered homing missile. Then contrasted the trajectories, control angles and loads of the missile with VSG and PNG (proportional navigation guidance) command order, and the simulation ...
null Feng Biming, null Song Jianjun
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SummaryIn this paper, a modified adaptive fast nonsingular terminal sliding mode guidance law is proposed based on the theory of fixed‐time convergence, which is applied for intercepting maneuvering targets considering terminal angle constraint. The proposed guidance law achieves system stabilization within bounded settling time independent on initial ...
Yao Zhang, Shengjing Tang, Jie Guo
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Terminal guidance with impact angle constraint based on a practical flight strategy
2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC), 2016The vehicle is expected to impact the target with high precision of position and direction while all the constraints are satisfied. First an optimal control model for terminal flight dynamics is formulated and the multi-shooting method is employed to obtain numerical optimal solutions.
null Wu Yanan +2 more
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Three‐dimensional predefined‐time sliding mode guidance with terminal angle constraints
Asian Journal of ControlAbstractGiven the shortness terminal guidance time, the convergence time of a guidance law is a key performance metric. To address this challenge and enhance the missile warheads' effectiveness, a three‐dimensional coupled nonlinear dynamic system with terminal line‐of‐sight (LOS) angle constraint is considered.
Yekun Liu +4 more
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Adaptive Terminal Sliding Mode Guidance Law with Impact Angle Constraint
2021 China Automation Congress (CAC), 2021Xin Yi, Ling Li, Haibin Zhao
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Non-singular terminal sliding mode cooperative guidance law under impact angle constraint
Journal of the Franklin InstitutezbMATH Open Web Interface contents unavailable due to conflicting licenses.
Fei Dong, Xiaoyu Zhang, Panlong Tan
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Spacecraft relative trajectory planning under terminal angle constraints via convex optimization
2022 China Automation Congress (CAC), 2022Zhang Runde +3 more
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Nonlinear three dimensional all-aspect guidance with terminal impact angle constraints
Aerospace Science and Technology, 2023Zhiwei Hou, Xuebin Zhuang, Hongbo Chen
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Excitonic devices with van der Waals heterostructures: valleytronics meets twistronics
Nature Reviews Materials, 2022Alberto Ciarrocchi +2 more
exaly
Prescribed Performance Terminal Sliding Mode based Guidance with Impact Angle Constraints
AIAA SCITECH 2023 Forum, 2023Kakoli Majumder, Shashi Ranjan Kumar
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