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| 1 | Recent advances in precision measurement & pointing control of spacecraft显示文摘There exists an increasing need for precision measurement&pointing control and extreme motion stability for current and future space systems,e.g.,Ultra-Performance Spacecraft(UPS).Some notable technologies of realizing Ultra-Pointing(UP)ability have been developed particularly for Ultra-accuracy Ultra-stability Ultra-agility(3 U)spacecraft over recent decades.Usually,Multilevel Compound Pointing Control Techniques(MCPCTs)are deployed in aerospace engineering,especially in astronomical observation satellites and Earth observation satellites.Modern controllers and/or algorithms,which are a key factor of MCPCTs for 3 U spacecraft,especially the jitter phenomena that commonly exist in a UPS Pointing Control System(PCS),have also been effectively used in some UP spacecraft for a number of years.Micro-vibration suppression approaches,however,are often proposed to deal with low-level mechanical vibration or disturbance in the microgravity environment that is common for UPS.This latter approach potentially is one of the most practical UP techniques for 3 U tasks.Some emerging advanced Disturbance-Free Payload(DFP)satellites that exploit the benefits of non-contact actuators have also been reported in the literature.This represents an interesting and highly promising approach for solving some challenging problems in the area.This paper serves as a state-of-the-art review of UP technologies and/or methods which have been developed,mainly over the last decade,specifically for or potentially could be used for 3 U spacecraft pointing control.The problems discussed in this paper are of reference significance to UPS and millisecond optical sensors,which are involved in Gaofeng Project,deep space exploration,manned space flight,and gravitational wave detection. | Lin LI Li YUAN Li WANG Ran ZHENG Yanpeng WU Xiaoyan WANG | 2021 | Chinese Journal of Aeronautics2021，34，10： | 8 |
| 2 | 基于改进迭代学习的参数不确定卫星姿态控制显示文摘针对卫星运行时存在的诸如在轨组装升级后的卫星转动惯量变化较大且难以确定等问题,提出一种基于改进预测迭代学习控制的姿态敏捷机动控制方法。首先,以改进递阶饱和控制作为反馈控制器,实现原系统的稳定。其次,加入改进预测迭代学习控制作为前馈控制器,提高系统动态性能、鲁棒性与敏捷性。然后,采用基于混合执行机构的零运动操纵律提供高精度大力矩,并解决控制力矩陀螺奇异和飞轮饱和问题。最后,通过仿真证明所提控制器的优越性。 | 柯晓曼 吴云华 郑墨泓 李文星 杜津铭 华冰 陈志明 | 2021 | 系统工程与电子技术2021，43，2： | 3 |
| 3 | Singularity radius gradient-based rapid singularity-escape steering law for SGCMGs显示文摘In order to visualize singularity of SGCMGs in gimbal angle space,a novel continuous bounded singularity parameter--Singularity Radius,whose sign can distinctly determine singularity type,is proposed.Then a rapid singularity-escape steering law is proposed basing on gradient of Singularity Radius and residual base vector to drive the SGCMG system to neighboring singular boundary,and quickly escape elliptic singularities.Finally,simulation results on Pyramid-type and skew-type configuration demonstrate the effectiveness and rapidness of the proposed steering law. | Tao YI Yunhai GENG Baolin WU | 2020 | Chinese Journal of Aeronautics2020，33，10： | 1 |
| 4 | A Poisson multi-Bernoulli mixture filter with spawning based on Kullback–Leibler divergence minimization显示文摘In the classical form,the Poisson Multi-Bernoulli Mixture(PMBM)filter uses a PMBM density to describe target birth,surviving,and death,which does not model the appearance of spawned targets.Although such a model can handle target birth,surviving,and death well,its performance may degrade when target spawning arises.The reason for this is that the original PMBM filter treats the spawned targets as birth targets,ignoring the surviving targets’information.In this paper,we propose a Kullback–Leibler Divergence(KLD)minimization based derivation for the PMBM prediction step,including target spawning,in which the spawned targets are modeled using a Poisson Point Process(PPP).Furthermore,to improve the computational efficiency,three approximations are used to implement the proposed algorithm,such as the Variational MultiBernoulli(VMB)filter,the Measurement-Oriented marginal MeMBer/Poisson(MOMB/P)filter,and the Track-Oriented marginal MeMBer/Poisson(TOMB/P)filter.Finally,simulation results demonstrate the validity of the proposed filter by using the spawning model in these three approximations. | Zhenzhen SU Hongbing JI Yongquan ZHANG | 2021 | Chinese Journal of Aeronautics2021，34，11： | 0 |
| 5 | 低轨卫星姿态控制系统降阶方案研究显示文摘近地卫星姿态控制单机故障会影响其任务的开展。针对低轨卫星姿控系统可能出现的单机故障情况,该文提出了姿态控制系统降阶方案,分别针对单飞轮故障、多飞轮故障、敏感器故障等不同场景,对姿态控制系统进行有序降阶,利用现有单机实现一定的姿态控制性能。单飞轮故障时采用轮速过零的三轴轮控方案;多飞轮故障且Y轮正常,或者高精度定姿单机故障时采用偏置稳定控制方案,在星体Y轴方向不能形成偏置时采用姿态控制方案。仿真结果表明,该文提出的针对各种单机故障情形的姿控方案均可较好地完成星体的姿态指向任务,卫星姿态控制系统可在单机出现故障时自主实施降阶方案。该文提出的姿态控制系统降阶方案可用作低轨卫星故障处理预案。 | 杜涵 许文彬 崔琦峰 李红 汤亮 | 2023 | 电子设计工程2023，31，8： | 0 |
| 6 | 基于反步法的空间目标复合指向控制方法研究显示文摘针对空间动目标高精度姿态跟踪控制问题,提出一种由卫星和二维转台组成的复合平台姿态高精度控制方法。首先建立复合平台耦合动力学模型,其次针对卫星本体设计反步法控制器实现粗跟踪。当姿态误差满足一定的切换要求时,粗跟踪误差作为二维转台的目标输入,二维转台采用基于负载观测器的模型预测方法辅助卫星本体进行姿态精跟踪控制,从而实现复合平台的高精度姿态控制。此外,设计了非线性干扰观测器,用来估计耦合运动对卫星本体产生的干扰力矩。数值仿真结果表明,所提出的复合平台姿态控制精度可以提高一个数量级,可以实现高精度姿态跟踪控制,为航天工程实践提供一定的理论基础。 | 张宏 吴云华 钟胜钧 郭海波 | 2023 | 系统工程与电子技术2023，45，9： | 0 |
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