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首页> 外文期刊>The Aeronautical Journal >Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation
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Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation

机译:具有执行器饱和度的冲击角约束拦截的自适应集成制导和控制

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摘要

This paper considers the integrated guidance and control (IGC) problem for impact angle constrained interception against manoeuvring targets with actuator saturation constraint. Based on the backstepping technique, an adaptive IGC law is presented to address this problem, where a fixed-time differentiator is proposed to estimate the derivatives of virtual control inputs to avoid the inherent problem of "explosion of complexity" suffered by the typical backstepping. Furthermore, an auxiliary first-order filter is introduced into the IGC law to cope with the actuator saturation constraint. The stability of the closed-loop system is strictly proved. Finally, the superiority of the proposed IGC law is verified by comparison simulations.
机译:本文考虑了针对具有执行器饱和约束的机动目标的冲击角约束拦截的集成制导和控制(IGC)问题。基于后推技术,提出了一种自适应IGC定律来解决该问题,其中提出了一个固定时间微分器来估计虚拟控制输入的导数,以避免典型后推所固有的“复杂性爆炸”问题。此外,将辅助一阶滤波器引入到IGC定律中,以应对执行器饱和约束。严格证明了闭环系统的稳定性。最后,通过比较仿真验证了提出的IGC定律的优越性。

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