空间天文望远镜自适应精密稳像闭环控制OA北大核心CSTPCD
Adaptive precision image stabilization control closed-loop method for space astronomical telescope
针对空间天文望远镜低频段视轴扰动补偿问题,提出了一种基于主动光学技术的自适应精密稳像闭环控制方法.该方法以精细导星仪(Fine Guide Sensor,FGS)为高精度视轴扰动检测器,以四点支撑压电驱动大口径快摆镜机构(Fast Steering Mirror,FSM)为视轴扰动补偿器.首先,采用位置式PID控制器串联积分环节进行精密稳像闭环控制,得到补偿FGS检测出的二维视轴扰动所需FSM的二维摆动角度,进而根据驱动结构转换为每个支撑点的压电陶瓷执行器(Piezoelectric actuators,PZT)的伸缩量.然后,利用基于广义Bouc-Wen逆模型的压电动态迟滞前馈补偿方法进行高精度的压电陶瓷执行器定位控制.最后,根据有监督的Hebb学习规则,利用具有自学习和自适应能力单神经元对PID控制器参数进行调整,从而得到最优控制器参数.实验结果表明,所提控制方法能够有效地补偿空间天文望远镜的视轴偏差,可以将精细导星仪X方向和Y方向的星点质心位置偏差功率谱密度在 0~6 Hz频段内积分值分别抑制了98.54%和98.62%.
An adaptive closed-loop control method for precision image stabilization based on active optical technology was proposed to compensate for low-frequency LOS disturbances in space astronomical tele-scopes.The fine guide sensor(FGS)was used as a high-precision LOS disturbance detector,and the four-point supporting large-aperture fast steering mirror(FSM)mechanism drove by piezoelectric actuators(PZT)was used as a LOS disturbance compensator in this method.First,a PID controller was connected in series with an integral link for precise image stabilization closed-loop control to obtain the two-dimen-sional swing angles of the FSM required to compensate for the two-dimensional LOS disturbance detected by FGS.Furthermore,the expansion amount of each PZT was calculated through driving structure.Then,the feedforward compensation method based on generalized Bouc-Wen inverse hysteresis model was used for high-precision positioning control of the piezoelectric ceramic actuator.Finally,according to supervised Hebb learning rules,the single neuron with self-learning and adaptive abilities was used to ad-just the PID controller parameters,thereby obtaining the optimal controller parameters.The experimental results show that the proposed control method can effectively compensate the LOS disturbance of the space astronomical telescope,and the integral value of PSD of the position error of the star point centroid in the X direction and Y direction of the FGS can be suppressed by 98.54%and 98.62%respectively in the frequency band of 0~6 Hz.
张泉;魏传新;高源蓬;朱雨霁;李清灵;房陈岩;周显宜;尹达一
中国科学院 红外探测与成像技术重点实验室,上海 200083||中国科学院 上海技术物理研究所,上海 200083
天文学
空间天文望远镜精密稳像精细导星仪大口径快摆镜机构迟滞补偿单神经元自适应PID控制
space astronomical telescopeprecision image stabilizationfine guide sensorfast steering mirrorhysteresis compensationsingle-neuron adaptive PID control
《光学精密工程》 2024 (008)
1153-1163 / 11
国家自然科学基金资助项目(No.12103075)
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