基于CFD的伞翼系统建模与控制

Wannan Wu, Qinglin Sun, Mingwei Sun, Zengqiang Chen
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引用次数: 0

摘要

在空投系统中,冠层气动参数的计算具有重要的意义。基于有限体积法,计算了翼伞系统的气动参数,并利用CFD输出数据估算了翼伞系统的偏转和切口因子。将所得的升力系数和阻力系数代替传统的升力线理论参数纳入伞翼系统的气动方程。采用自抗扰控制策略对系统进行控制。仿真结果验证了该方法的有效性。本文的工作可为伞翼系统的设计提供参考。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Modeling and Control of Parafoil Systems Based on CFD
The calculation of canopy aerodynamic parameters plays an important part in the airdrop system. Based on the finite volume method, this paper calculates the aerodynamic parameters of the parafoil systems, and then the deflection and incision factors are estimated by the CFD output data. The obtained lift and drag coefficients instead of the traditional parameters based on lifting-line theory are incorporated into the aerodynamic equation of a parafoil system. The active disturbance rejection control strategy is applied to control the systems. The effectiveness of the proposed method can be demonstrated by the simulation results. The work in this paper may be a reference for the parafoil system design.
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