摘要
针对低空掠海飞行拖靶建模误差和外界扰动大的特点,提出了自抗扰高度控制律设计方法。该方法通过安排过渡过程解决了超调与快速性的矛盾,跟踪微分器提取误差的微分信号有效实现了微分反馈,非线性反馈在避免使用积分器的同时提高了控制效率。采用扩张状态观测器对未建模动态和干扰作用进行估计并补偿。仿真结果表明,在存在模型摄动和外界扰动情况下,基于自抗扰控制的拖靶高度控制系统具有较好的动态品质、稳态精度以及较强的鲁棒性。
To solve the problems that the modeling error and the internal and external disturbances of the low altitude sea-skimming tow target are great, an altitude control scheme based on the active dis- turbance rejection control technique is proposed. The contradiction of over-control and rapidity is harmonized by arranging the transient process, and the feedback of differential signal is achieved by track differentiator extracting the differential error signal. A nonlinear feedback method is used to improve the control efficiency avoid using integrator. Finally, the un-modeled dynamics and unknown disturbances in the system are estimated and compensated by the extended-state observer. The simulation results show that the control system has good dynamic capability, stable precision and strong robustness when being imported several kinds of disturbances.
出处
《南京理工大学学报》
EI
CAS
CSCD
北大核心
2012年第5期835-839,845,共6页
Journal of Nanjing University of Science and Technology
关键词
拖靶
自抗扰控制
跟踪微分器
非线性反馈
扩张状态观测器
tow targets
active disturbance rejection control
track differentiators
nonlinearfeedback
extended-state observers