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首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers >Longitudinal automatic carrier landing system guidance law using model predictive control with an additional landing risk term
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Longitudinal automatic carrier landing system guidance law using model predictive control with an additional landing risk term

机译:纵向航母自动着陆系统制导律,使用模型预测控制及附加着陆风险项

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This paper used a model predictive control with an additional term to develop a modified longitudinal guidance law to reduce landing risk in an automatic carrier landing system. The landing risk model was established by using a longitudinal trajectory and touchdown point predictive principle. A traditional MPC was then involved in designing a modified automatic carrier landing system guidance law for the proposed model. The nonlinear landing mathematic model of an F/A-18 carrier-based aircraft was initially established. Considering the processed procedure in the model predictive control algorithm, the corresponding linear landing model was derived on the basis of the equilibrium states of the F/A-18. Second, landing trajectory in the longitudinal plane was analysed so that the predictive principle of the trajectory trend was reasonably addressed. Depending on the experimental sample data of a pilot model, some linear imitating envelopes are transformed from the corresponding nonlinear trajectory clusters. Furthermore, a touchdown point prediction model was further established based on the predicted trajectory and touchdown point. Third, the traditional model predictive control was introduced to integrate the landing risk term in the performance cost function to develop a novel modified algorithm that not only guides the aircraft to automatically approach and land on the carrier, but also eliminates landing risk during the final carrier approach. Linear matrix inequalities were imported to substitute algebraic inequalities derived from this new algorithm to increase calculating speed. A simulation mission was conducted on a semi-physical platform and compared with the traditional model predictive control without the additional term. The theoretical results validated the correctness and robustness of the modified algorithm and its capability to eliminate landing risk during terminal carrier approach.
机译:本文使用了带有附加术语的模型预测控制来开发修正的纵向制导律,以降低自动航母着陆系统中的着陆风险。利用纵向轨迹和着陆点预测原理建立了登陆风险模型。然后,传统的MPC参与了为所提议模型设计的修改后的自动航母着陆系统制导律。最初建立了F / A-18舰载飞机的非线性着陆数学模型。考虑到模型预测控制算法中的处理过程,根据F / A-18的平衡状态得出了相应的线性着陆模型。其次,分析了纵向平面上的着陆轨迹,从而合理地说明了轨迹趋势的预测原理。根据试验模型的实验样本数据,从相应的非线性轨迹簇转换一些线性模拟包络。此外,基于预测的轨迹和着陆点,进一步建立了着陆点预测模型。第三,引入了传统的模型预测控制,以将着陆风险项整合到性能成本函数中,以开发出一种新颖的改进算法,该算法不仅可以指导飞机自动接近并降落在航母上,而且可以消除最终航母的着陆风险方法。引入线性矩阵不等式来替代从该新算法得出的代数不等式,以提高计算速度。在半物理平台上执行了模拟任务,并将其与不带附加项的传统模型预测控制进行了比较。理论结果验证了改进算法的正确性和鲁棒性以及消除终端航母进近过程中着陆风险的能力。

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