Autopilot Design Method for the Blended Missile Based on Model Predictive Control
Autopilot Design Method for the Blended Missile Based on Model Predictive Control
复制标题
基于模型预测控制的混合导弹自动驾驶仪设计方法
DOI：
10.1155/2015/718036
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发表时间：
2015-02
影响因子：
1.4
通讯作者：
Zhao Yuyu
中科院分区：
文献类型：
--
作者：
Yang Baoqing;Zhao Yuyu
This paper develops a novel autopilot design method for blended missiles with aerodynamic control surfaces and lateral jets. Firstly, the nonlinear model of blended missiles is reduced into a piecewise affine (PWA) model according to the aerodynamics properties. Secondly, based on the equivalence between the PWA model and mixed logical dynamical (MLD) model, the MLD model of blended missiles is proposed taking into account the on-off constraints of lateral pulse jets. Thirdly, a hybrid model predictive control (MPC) method is employed to design autopilot. Finally, simulation results under different conditions are presented to show the effectiveness of the proposed method, which demonstrate that control allocation between aerodynamic control surfaces and lateral jets is realized by adjusting the weighting matrix in an index function.
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DOI：
10.2514/6.1998-4494
发表时间：
1998-08
期刊：
--
影响因子：
--
作者：
P. Menon;V. R. Iragavarapu
通讯作者：
P. Menon;V. R. Iragavarapu
影响因子：
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作者：
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发表时间：
2007-08
期刊：
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影响因子：
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D. Ridgely;D.T. Drake;L. Triplett;Cory Geise
影响因子：
6.8
作者：
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