Transactions of Nanjing University of Aeronautics & Astronautics
LPV Flight Dynamics Modeling for Turbulent Wind Special Flight Analysis
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Abstract:
A linear parameter varying (LPV) flight dynamics model (FDM) is proposed to cater for atmospheric disturbance analysis in special flight conditions. A novel FDM which is capable of addressing the influence of turbulent wind is derived under the wind frame. An affine parameter dependent LPV model with wind effects is built based on function substitution method. The optimal solution for the decomposing function of the LPV FDM is obtained by genetic algorithm (GA). The analysis of dynamic response indicates that the genetic-optimized LPV FDM approximates the nonlinear FDM evidently, since it identifies the instantaneous dynamics and flight states varying in a wide range. The simulations of approach and landing against wind shear show that the genetic-optimized LPV FDM captures the instantaneous dynamic response when flying through turbulent wind, indicating that the LPV model can be further applied to turbulent wind special flight analysis and control law design.
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This work was supported by the National Natural Science Foundation of China (No.U1533120),the Aeronautical Science Foundation of China (No. 20158052057),and the Fundamental Research Funds for the Central Universities(No.NS2015066).
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