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排序方式: 共有453条查询结果,搜索用时 46 毫秒
91.
92.
为了分析大气阻力摄动对卫星编队队形的影响,利用相对轨道根数法推导了包含大气阻力摄动的卫星编队相对运动的状态转移方程。仿真结果表明当几何形状和质量不同的两颗卫星在低轨道做编队飞行时,大气阻力摄动对编队队形的影响很大而不能忽略;当主卫星的半长轴相等时,主卫星轨道的偏心率越大编队飞行受大气阻力摄动的影响也越大;大气阻力摄动主要影响编队飞行迹向相对距离。 相似文献
93.
文章全面分析了TDICCD相机相对孔径选择的几个因素,与近年通常只考虑地面分辨率、MTF、S/N和像移的影响,较少涉及图像混叠对像质影响不同,文章重点提出混叠对D/f选择的影响,并计算得出理想条件下遥感系统参数的最佳值。 相似文献
94.
Vasileios Tserolas Stelios P. Mertikas Xenophon Frantzis 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
The Global Positioning System makes it possible, nowadays, to measure crustal displacements with unprecedented accuracy. These measurements can improve our understanding of the spatio-temporal evolution of motion along tectonic plate boundaries, as well as deepen our comprehension for the nature of earthquake fault behavior and earthquake cycle. The Hellenic subduction zone and the earthquake-prone Crete, with large crustal motions of 3–4 cm/yr, may provide such a natural laboratory for this type of investigation. In this work, we examine the statistical structure and behavior of time series, as produced by permanent GPS sites, established on the islands of Crete and Gavdos. 相似文献
95.
The capacity to acquire the relative position and attitude information between the chaser and the target satellites in real time is one of the necessary prerequisites for the successful implementation of autonomous rendezvous and docking. This paper addresses a vision based relative position and attitude estimation algorithm for the final phase of spacecraft rendezvous and docking. By assuming that the images of feature points on the target satellite lie within the convex regions, the estimation of the relative position and attitude is converted into solving a convex optimization problem in which the dual quaternion method is employed to represent the rotational and translational transformation between the chaser body frame and the target body frame. Due to the point-to-region correspondence instead of the point-to-point correspondence is used, the proposed estimation algorithm shows good performance in robustness which is verified through computer simulations. 相似文献
96.
《北京航空航天大学学报》2012,38(2)
以机载泵源系统的恒功率控制为目标,针对作业任务中系统负载随时间变化的情况,采用使液压系统输出功率保持恒定的控制方式来达到充分利用发动机功率的目的,对于机载泵源控制系统的主要被控对象——轴向柱塞式变量泵,建立了其状态方程和流量输出方程,采用H。鲁棒镇定控制策略实时调节泵的排量,仿真结果表明:当负载变化时,系统能根据压力的变化快速转换到恒功率工作曲线下对应的流量状态,所设计的H。控制器能够减小干扰和模型参数不确定对系统稳定性的影响,具有良好的鲁棒性,表明该方法用于机载液压系统可以改善系统工作性能,提高系统功率的利用率。 相似文献
97.
Stability and shape analysis of relative equilibrium for three-spacecraft electromagnetic formation 总被引:1,自引:0,他引:1
The invariant shapes for close formation flying with inter-craft electromagnetic force ensure several potential space applications. However, the 6-DOF relative equilibrium problem has not been systematically investigated. This paper mainly analyzes the invariant shapes of relative equilibrium for the three-spacecraft electromagnetic formation, and studies the families of invariant shape solutions with real and constant magnetic moments as well as their linear stability. The problem is examined based on the full nonlinear coupled dynamic models for collinear and general triangular configurations. The relative equilibrium conditions are analyzed to determine whether an invariant shape do exist, and the corresponding families of invariant shape solutions are identified for static and spinning configurations respectively. Finally, the linear stability of such invariant shapes is numerically discussed, which have shown that most invariant shapes are unstable and controllable. 相似文献
98.
《中国航空学报》2020,33(8):2242-2256
In cabin-type component alignment, digital measurement technology is usually adopted to provide guidance for assembly. Depending on the system of measurement, the alignment process can be divided into measurement-assisted assembly (MAA) and force-driven assembly. In MAA, relative pose between components is directly measured to guide assembly, while in force-driven assembly, only contact state can be recognized according to measured six-dimensional force and torque (6D F/T) and the process is completed based on preset assembly strategy. Aiming to improve the efficiency of force-driven cabin-type component alignment, this paper proposed a heuristic alignment method based on multi-source data fusion. In this method, measured 6D F/T, pose data and geometric information of components are fused to calculate the relative pose between components and guide the movement of pose adjustment platform. Among these data types, pose data and measured 6D F/T are combined as data set. To collect the data sets needed for data fusion, dynamic gravity compensation method and hybrid motion control method are designed. Then the relative pose calculation method is elaborated, which transforms collected data sets into discrete geometric elements and calculates the relative poses based on the geometric information of components. Finally, experiments are conducted in simulation environment and the results show that the proposed alignment method is feasible and effective. 相似文献
99.
《中国航空学报》2020,33(1):365-371
The variable pump displacement and variable motor speed electro-hydrostatic actuator (EHA), one of the three types of EHAs, has advantages such as short response time, flexible speed regulation, and high efficiency. However, the nonlinearity of its double-input single-output system poses a great challenge for system control. This study proposes a novel EHA with adaptive pump displacement and variable motor speed (EHA-APVM). A closed-loop position is realized using a servomotor. Moreover, the displacement varies with the system pressure; thus, the EHA-APVM is a single-input and single-output system. Firstly, the working principles of the EHA-APVM and the pump used in the system are introduced. Secondly, a nonlinear mathematical model of the proposed EHA-APVM control system is established, and a feedback back-stepping (FBBS) control algorithm is introduced to transform the complex nonlinear system into a linear system on the basis of the back-stepping control theory. Finally, simulation results prove that the EHA-APVM has a quick response and high robustness to variations of the load and the pump displacement. In this work, the size and weight of the motor are significantly reduced because the maximum power requirement is reduced, which is very beneficial for using the actuator in airborne equipment. 相似文献
100.
姜旻 《南京航空航天大学学报》2000,32(4):465-468
不等距的窄槽载正加工是机械加工的难题之一。文中采用了电涡流传感器来采集窄槽的位置信号,利用信号边沿部分对称的特点,采用了“倒序列相关”的方法 用倒序信号与原信号进行互相关分析,充分利用了信号的全过程,滤除了信号中的随机成分,精确地求得窄槽的中心位置。试验的结果与理论研究基本相符,表明此方法具有实用价值。 相似文献