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首页> 外文期刊>International journal of aerospace engineering >Discrete-Time Angle Constraint Interception with Model-Assisted Target Maneuver Estimator
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Discrete-Time Angle Constraint Interception with Model-Assisted Target Maneuver Estimator

机译:模型辅助目标机动估算器的离散时间角约束拦截

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This paper investigates the problem of designing angle constraint guidance law against unknown maneuvering targets based on discrete-time sliding mode control theory. Invoking the fact that the future course of action of the target, an independent entity, cannot be predicted beforehand due to its complexity and unpredictability, a model-assisted discrete-time disturbance observer in cooperation with a singularity-free strategy is proposed first to estimate the target maneuver. Based on the reconstructed signal and a fast convergence time-varying sliding surface, a new chattering-mitigated super-twisting-like discrete-time impact angle constraint guidance law is then synthesized. Stability analysis shows that the closed-loop system trajectory can be forced to enter into a small region around the sliding surface. Simulations and comparisons with classical discrete-time sliding mode guidance law validate the effectiveness of the proposed guidance law.
机译:本文研究了基于离散时间滑动模式控制理论的针对未知机动目标设计角度约束指导法的问题。援引目标的未来行动课程是由于其复杂性和不可预测性无法预测,无法预测独立的实体,首先提出了一种与奇点战略合作的模型辅助的离散时间扰动观察者来估算目标机动。基于重建信号和快速收敛时变滑动表面,然后合成了一种新的抖动缓解的超扭曲的离散时间冲击角约束指导法。稳定性分析表明,闭环系统轨迹可以被迫进入滑动表面周围的小区域。仿真和比较经典离散时间滑模指导法验证了拟议的指导法的有效性。

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