ID 原文 译文
11664 通过姿态稳定控制,用反作用飞轮反馈的力矩信息,实时计算出模拟器质心位置。 ‭Through the attitude stability control, using reaction flywheel torque feedback information, real-time calculate the barycentric position of the simulator.
11665 通过控制3个正交的配平系统,补偿质心位置偏差。 ‭By controlling the three orthogonal balancing system, compensation centroid position deviation.
11666 根据实验测得的回路参数,优化设计配平系统控制律。 ‭Measured according to the experiment of the circuit parameter, optimization control law design of balancing system.
11667 将跟踪微分器应用于力矩信息处理,有效减少电机反复运动,提高配平效率。 ‭The tracking differentiator is applied to torque information processing, effectively reduce motor sports repeatedly, improve the efficiency of balancing.
11668 提出的配平方法成功用于航天器三自由度模拟器的实验中。 ‭The balancing method is successfully used in spacecraft three degree of freedom simulation experiment. ‭
11669 为了提高控制系统状态估计的快速性并保证其准确性,将重置控制的思想引入观测器设计,即当观测器满足预先设定的重置条件时将其状态进行重置,提出了一种新型自适应重置观测器设计方法。 In order to improve the rapidity of control system based on state estimation and ensure its accuracy, will reset the observer design idea of the control, namely when the observer meet preset reset condition will be reset, its state is put forward a new kind of reset adaptive observer design method.
11670 重置观测器能够克服线性反馈方式的内在局限性,可实现同时降低估计误差的超调量与调节时间。 Reset the observer is able to overcome the inherent limitations of linear feedback way, can be realized at the same time reduce the overshoot and adjustment time estimation error.
11671 首先对重置积分项引入自适应参数,并基于过零重置条件设计自适应重置观测器。 The adaptive parameter is introduced to reset the integral term, and based on the zero reset condition reset adaptive observer design.
11672 对于含有重置项的自适应观测器,通过基于Lyapunov函数的方法对其进行稳定性分析,并整理成线性矩阵不等式的形式,使得设计过程更为简便、易于实现。 For adaptive observer contains reset item, based on Lyapunov function method for stability analysis, and collates them into the form of linear matrix inequality (lmi), makes the design process more simple and easy to implement.
11673 最后通过与比例积分观测器进行比较,验证了所提方法的有效性与优越性。 At last, by comparing with proportional integral observer, verify the effectiveness and superiority of the proposed method.