基于对偶四元数的卫星信息一致性控制

为了解决航天器控制信息一致性问题,提出了利用对偶四元数来描述对象的位置及姿态信息,实现位置与姿态的统一表述。同时利用信息一致性理论,通过设计航天器间的信息传递模型来解决分布式航天器间的状态同步问题。采用对偶四元数及信息一致性理论为工具,分别给出了位姿同步及跟踪两种控制方法并针对两种信息拓扑模型,以空间交会对接问题进行仿真实验,实验结果表明,在500s以内,卫星的位置及姿态实现了同步及跟踪控制。     

单目视觉下基于对偶四元数的卫星姿态的确定

在航天器姿态动力学和机器视觉理论基础上,提出一种新的卫星姿态确定的算法。单目相机作为观测设备,用对偶四元数以及几何透视投影法,将从星3D姿态参数转换为2D照片平面参数。最后,将表征坐标变换的对偶四元数中的位移和旋转分量以及运动角速度和线速度作为状态量,2D坐标参数作为观测值,建立滤波器,得到了表示相对运动的对偶四元数的估计值。在30s内的仿真结果证明了对偶四元数在表示刚体运动变换时的优越性,为从星姿态测量找到一个更有工程应用价值的方法。     

Continuous non-autonomous memristive Rulkov model with extreme multistability

Based on the two-dimensional (2D) discrete Rulkov model that is used to describe neuron dynamics, this paper presents a continuous non-autonomous memristive Rulkov model. The effects of electromagnetic induction and external stimulus are simultaneously considered herein. The electromagnetic induction flow is imitated by the generated current from a flux-controlled memristor and the external stimulus is injected using a sinusoidal current. Thus, the presented model possesses a line equilibrium set evolving over the time. The equilibrium set and their stability distributions are numerically simulated and qualitatively analyzed. Afterwards, numerical simulations are executed to explore the dynamical behaviors associated to the electromagnetic induction, external stimulus, and initial conditions. Interestingly, the initial conditions dependent extreme multistability is elaborately disclosed in the continuous non-autonomous memristive Rulkov model. Furthermore, an analog circuit of the proposed model is implemented, upon which the hardware experiment is executed to verify the numerically simulated extreme multistability. The extreme multistability is numerically revealed and experimentally confirmed in this paper, which can widen the future engineering employment of the Rulkov model.