Horizontal Path-following Control Based on ESO for Parafoil Systems with Error Constraint

Erlin Zhu, Youwu Du, Haitao Gao, W. Song
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Abstract

This paper investigates the problem of horizontal path-following control for parafoil systems with error constraint. Frist, by introducing the guidance theory, the horizontal position control is converted to the control of the azimuth angle of the parafoil system. The error signal of the angle is transformed to a new error variable, such that the error is constrained into the prescribed boundaries. Next, the methods of backstepping and output feedback are employed in the controller design. The uncertainties in parafoil system modeling and external disturbances are estimated using the lineaer extended state observer (LESO). The stability analysis based on Lyapunov method shows that all the error signals are uniformly ultimately bounded. Simulation results of a 6 degree-of-freedom parafoil system illustrate the effectiveness of the proposed method.
基于ESO的误差约束伞系统水平路径跟踪控制
研究了带误差约束的伞翼系统的水平路径跟踪控制问题。首先,通过引入制导理论,将水平位置控制转化为伞翼系统方位角的控制。将角度误差信号转化为新的误差变量,使误差约束在规定的边界内。其次,采用反步法和输出反馈法进行控制器设计。利用线性扩展状态观测器(LESO)对伞翼系统建模中的不确定性和外界干扰进行估计。基于Lyapunov方法的稳定性分析表明,所有误差信号最终都是一致有界的。对六自由度伞翼系统的仿真结果验证了该方法的有效性。
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