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具有输入输出约束的无人直升机预设性能安全跟踪控制

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针对无人直升机姿态与高度系统存在未知外部干扰、输入饱和、姿态与高度约束等问题,本文提出一种具有输入输出约束的预设性能安全跟踪控制方法。首先,针对无人直升机的姿态与高度约束,通过设计一类边界保护算法,构建了新的安全期望跟踪信号。为了保证系统对于安全期望跟踪信号的跟踪性能,将预设性能函数与边界保护算法进行结合,并对跟踪误差进行转换。针对系统的输入饱和现象,使用Sigmoid函数进行逼近;同时,针对饱和函数的逼近误差与未知外部干扰构成的复合干扰,采用参数自适应方法对其上界进行逼近。然后,结合反步控制方法设计了安全跟踪控制器,并通过Lyapunov稳定性理论证明了闭环系统所有信号的收敛性,保证了无人直升机的安全跟踪性能。最终,通过数值仿真验证了所提控制方法的有效性。
Prescribed performance safe tracking control for the unmanned helicopter with input and output constraints
This paper deals with the problem of prescribed performance safe tracking control for the attitude and alti-tude system of unmanned helicopter with unknown external disturbances,input saturation,and constraints of attitude and altitude.Firstly,by considering the constraints of attitude and altitude,a safe desired tracking signal is constructed with the application of an output boundary protection algorithm.Furthermore,combining with the proposed output boundary protection algorithm,the prescribed performance function is developed to guarantee the tracking performance of the safe desired tracking signal.A Sigmoid function is utilized to tackle the problem of saturation input.To compensate the com-pound disturbances which include external disturbances and the estimation error of Sigmoid function,a parameter adaptive method is adopted to approximate its upper bound.Combining with the backstepping technology,the safe tracking con-troller is investigated.The Lyapunov stability theory is employed to guarantee the boundedness of all closed-loop signals and the safe tracking performance of the unmanned helicopter system.Simulation results of an example are provided to illustrate the effectiveness of the proposed control scheme.

unmanned helicoptersafe controlprescribed performanceadaptive controlinput saturation

马浩翔、陈谋、吴庆宪

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南京航空航天大学自动化学院,江苏南京 211106

河南科技大学信息工程学院,河南洛阳 471023

无人直升机 安全控制 预设性能 自适应控制 输入饱和

国家自然科学基金国家杰出青年科学基金江苏省重点研发计划(社会发展项目)

U201320161825302BE2020704

2024

控制理论与应用
华南理工大学 中国科学院数学与系统科学研究院

控制理论与应用

CSTPCD北大核心
影响因子:1.076
ISSN:1000-8152
年,卷(期):2024.41(1)
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