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Effect of Estimation on the Performance of an Integrated Missile Guidance and Control System

机译:估算对导弹制导与控制系统综合性能的影响

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摘要

Motivated by spectral separation, guidance and control systems of interceptors are traditionally designed separately. However, interception of highly maneuverable targets and increased interception accuracy requirements lead to intense maneuvering during the last phase of the engagement, thus violating the spectral separation assumption of the conventional two-loop design. This has boosted the interest in integrated guidance-control designs that demonstrate superior interception accuracies by accounting for the coupling between the kinematics and dynamics of the problem. One of the approaches used for the integrated design is the sliding mode control (SMC) methodology. The results presented so far assumed full state information. We examine the effect of estimation on the performance of the integrated sliding mode controller design. In particular, a sliding mode observer/differentiator (SMOD) is used to estimate the target states. Through an intensive numerical study it is shown that the integrated guidance-control approach has a clear advantage over a conventional separated two-loop design. This advantage is attributed to the robustness of the integrated sliding mode controller design that better deals with the estimation errors and measurements noises.
机译:受光谱分离的影响,拦截器的制导和控制系统传统上是分开设计的。然而,高度机动的目标的拦截和增加的拦截精度要求导致在接合的最后阶段进行激烈的机动,从而违反了常规两环设计的光谱分离假设。通过考虑问题的运动学和动力学之间的耦合,这提高了人们对集成制导控制设计的兴趣,该设计显示了出色的拦截精度。用于集成设计的方法之一是滑模控制(SMC)方法。到目前为止,给出的结果均假定了完整的状态信息。我们研究了估计对集成滑模控制器设计性能的影响。特别地,滑模观察器/微分器(SMOD)用于估计目标状态。通过大量的数值研究表明,与传统的分离式两回路设计相比,集成制导控制方法具有明显的优势。该优势归因于集成滑模控制器设计的耐用性,该设计可以更好地处理估计误差和测量噪声。

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