Title of article
Guidance law for low-lift skip reentry subject to control saturation based on nonlinear predictive control
Author/Authors
Minwen، نويسنده , , Guo and Dayi، نويسنده , , Wang، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2014
Pages
7
From page
48
To page
54
Abstract
A novel guidance law is presented for low-lift skip reentry. The law is developed based on nonlinear predictive control theory. Firstly, an output vector is carefully chosen. In the framework of nonlinear predictive control, the predicted output tracking errors are viewed as the performance index. Then, a single-input–multiple-output guidance law is derived by minimizing that index even in the presence of the control saturation. The most prominent advantage of this approach is that the selected output vector is able to improve the accuracy of reentry landing. Moreover, the stability and robustness of the designed guidance law are analyzed. Simulation results are presented to verify the effectiveness and robustness of the law with respect to parameter uncertainties when comparing with the feedback linearization theory based guidance law.
Keywords
Control Saturation , robustness analysis , nonlinear predictive control , Parameter uncertainties , Low-lift skip reentry
Journal title
Aerospace Science and Technology
Serial Year
2014
Journal title
Aerospace Science and Technology
Record number
2231371
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