首页|期刊导航|空间控制技术与应用(中英文)|多级航天器高精度六自由度相对控制方法研究

多级航天器高精度六自由度相对控制方法研究OA

High-Precision Six-Degree-of-Freedom Relative Control Method for Multi-stage Spacecraft

中文摘要英文摘要

针对空间分布式干涉测量任务中,相对测量敏感器因力热环境存在缓变漂移以及主动指向超静平台缺乏平动主动控制的问题,开展多级航天器六自由度高精度相对位姿控制方法研究.利用超静平台具备的六维力输出能力,提出一种集状态估计与多级协同抗扰于一体的控制方案.基于增广卡尔曼滤波设计相对平动状态估计器,实现了对敏感器空间缓变漂移的在线实时估计与精确补偿.针对平台结构的六自由度强耦合干扰,将平动方向的主动控制回路融入多级协同抗扰控制器设计,消除了平动与姿态自由度间的动态耦合影响.仿真与理论分析表明,该方案能够有效抑制空间复杂扰动,使系统相对位置与姿态控制精度分别达到微米和亚角秒级.研究成果可为分布式空间干涉测量任务中超高精度编队系统的工程实现提供技术参考.

To address the issues of slow sensor drift caused by thermal-mechanical environments and the lack of active translational control in active pointing ultra-quiet platforms during distributed space interferometry missions,a six-degree-of-freedom(6-DOF)high-precision relative position and attitude control method for multi-stage spacecraft is investigated.Utilizing the six-dimensional force output capability of the ultra-quiet platform,an integrated control scheme combining state estimation and multi-stage coordinated anti-disturbance is proposed.First,an augmented Kalman filter-based relative translational state estimator is designed to explicitly estimate and compensate for the sensor's slow drift in real time.Subsequently,to tackle the severe 6-DOF dynamic coupling inherent in the platform structure,an active translational control loop is incorporated into the multi-stage coordinated anti-disturbance controller,eliminating the dynamic coupling between the translational and attitude degrees of freedom.Simulation and theoretical analysis demonstrate that the proposed strategy effectively suppresses complex space disturbances,achieving micrometer relative positioning and sub-arcsecond pointing accuracies.The research findings provide a critical technical reference for the engineering implementation of ultra-high-precision formation systems in future distributed space interferometry missions.

宋继良;郝仁剑;汤亮;王有懿

北京控制工程研究所,北京 100094||空间智能控制全国重点实验室,北京 100094北京控制工程研究所,北京 100094||空间智能控制全国重点实验室,北京 100094北京控制工程研究所,北京 100094||空间智能控制全国重点实验室,北京 100094北京控制工程研究所,北京 100094||空间智能控制全国重点实验室,北京 100094

航空航天

多级航天器主动指向超静平台六自由度控制增广卡尔曼滤波抗扰控制

multi-stage spacecraftactive pointing ultra-quiet platform6-DOF controlaugmented Kalman filteranti-disturbance control

《空间控制技术与应用(中英文)》 2026 (4)

33-42,10

国家自然科学基金资助项目(U23B6002) National Natural Science Foundation of China(U23B6002)

10.3969/j.issn.1674-1579.2026.04.004

评论