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采用指令前馈补偿的卫星高精度指向跟踪复合控制方法

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提出了基于目标相对运动轨迹的前馈补偿+闭环反馈的复合控制方法,以大幅改善卫星动态指向跟踪控制精度.首先,采用动态误差系数法和功率传递函数,分别从指向跟踪误差和敏感器测量噪声引起的稳定度偏差两个方面分析了反馈带宽的选取范围.然后,依据跟踪误差传递函数模型,提出了通过相对导航滤波计算目标星视线角速度和角加速度的前馈补偿控制策略,解决了由于星载探测设备仅能测量目标指向偏差信息,而无法直接进行复合控制的难题.最后,通过数学仿真验证系统的稳定性和姿态跟踪性能,并设计了地面气浮台试验对控制器的跟踪性能进行测试.该姿态控制器能够在不改变闭环反馈带宽的前提下,实现对不同输入指令下高精度动态跟踪.
A Composite Control Method for High-Precision Satellite Pointing Tracking by Command Feedforward Compensation
A hybrid control method combining feed-forward compensation with closed-loop feedback based on the target relative motion trajectory is proposed in this paper,which is aiming at significantly improving the satellite dynamic pointing tracking control precision.Firstly,the dynamic error coefficient method is a-dopted to analyze the attitude tracking errors,and power transfer function is established to analyze attitude angular velocity errors caused by sensor noise.Next,a feed-forward compensation control strategy calculat-ing the desired line-of-sight angular velocity and angular acceleration by estimation of the target relative motion is proposed,which resolves the challenge of space-borne detection equipment that can only measure target pointing deviations and doesn't directly perform hybrid control.Finally,the system stability and at-titude tracking performance are validated through mathematical simulations,and ground-based air-bearing experiments are implemented to test the controller's tracking performance.This attitude controller reaches high-precision during dynamic tracking by different input commands without altering the closed-loop feed-back bandwidth.

Pointing tracking controlNoise suppressionRelative navigation filteringFeed-forward compensationAir-bearing experiment

郭正勇、王静吉、黄京梅、戴维宗、王北超、李爽

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南京航空航天大学航天学院,南京 211106

上海航天控制技术研究所,上海 201109

指向跟踪控制 噪声抑制 相对导航滤波 前馈补偿 气浮台试验

2024

航天控制
北京航天自动控制研究所

航天控制

CSTPCD
影响因子:0.29
ISSN:1006-3242
年,卷(期):2024.42(6)