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A variable structure passivity control method for elastic joint robots based on cascaded high-order state estimation
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作者 ZHANG JieXin nie pingyun ZHANG Bo 《Science China(Technological Sciences)》 SCIE EI CAS CSCD 2024年第2期395-407,共13页
Passivity-based controllers are widely used to facilitate physical interaction between humans and elastic joint robots,as they enhance the stability of the interaction system.However,the joint position tracking perfor... Passivity-based controllers are widely used to facilitate physical interaction between humans and elastic joint robots,as they enhance the stability of the interaction system.However,the joint position tracking performance can be limited by the structures of these controllers when the system is faced with uncertainties and rough high-order system state measurements(such as joint accelerations and jerks).This study presents a variable structure passivity(VSP)control method for joint position tracking of elastic joint robots,which combines the advantages of passive control and variable structure control.This method ensures the tracking error converges in a finite time,even when the system faces uncertainties.The method also preserves the passivity of the system.Moreover,a cascaded observer,called CHOSSO,is also proposed to accurately estimate high-order system states,relying only on position and velocity signals.This observer allows independent implementation of disturbance compensation in the acceleration and jerk estimation channels.In particular,the observer has an enhanced ability to handle fast time-varying disturbances in physical human-robot interaction.The effectiveness of the proposed method is verified through simulations and experiments on a lower limb rehabilitation robot equipped with elastic joints. 展开更多
关键词 motion control elastic joint robot finite-time convergence high-order system state estimation physical human-robot interaction
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基于模型预测控制的固体火箭发动机多阀协同控制方法
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作者 宗志强 李睿 +3 位作者 姜天祥 聂平芸 牛禄 张波 《机械与电子》 2024年第11期23-31,共9页
为实现固体火箭发动机推力的快速、精确调节,提出一种基于模型预测控制的多燃气阀协同控制方法。该方法基于发动机推力的单增量模型预测发动机推力的跟踪误差,考虑燃气阀的开度范围约束,通过滚动时域优化求解各燃气阀的参考速度。相比... 为实现固体火箭发动机推力的快速、精确调节,提出一种基于模型预测控制的多燃气阀协同控制方法。该方法基于发动机推力的单增量模型预测发动机推力的跟踪误差,考虑燃气阀的开度范围约束,通过滚动时域优化求解各燃气阀的参考速度。相比于现有方法,所提方法根据燃气阀开度反馈实时修正参考速度,实现了发动机推力的闭环控制,有效抑制了扰动对多阀协同控制性能的影响。此外,该方法较现有方法可以实现更大的推力调节范围。最后,基于多燃气阀协同控制实验平台验证了所提方法的可行性和有效性。 展开更多
关键词 多阀协同控制 推力调控 固体火箭发动机 模型预测控制
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