24 resultados para motion analysis

em Chinese Academy of Sciences Institutional Repositories Grid Portal


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为分析空间电动绳系的运动特性,从一般力学角度出发,结合电动力学知识,建立了近地轨道空间电动绳系推进飞行的动力学模型,得出了多种初始条件下的数值计算结果,并据此对电动绳系航天器的轨道机动过程进行了详尽的讨论,阐明了系统在轨道高度变化的同时,其轨道面也会发生变化,而且导电系绳还会旋转与弯曲变形等规律.此外,还对电动绳系推进系统的效率和地球自转的影响进行了估计.

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提出并研制一种基于自适应移动机构的管内探查机器人。通过对机器人传动机构的设计,实现了在不增加驱动电动机数量的前提下,机器人具有适应不同管道直径的能力。机器人的传动机构能够在管道直径改变时,自动地改变行走部件的输出形式以克服障碍,完成越障任务。在没有应用链式多节构型的情况下,机器人配备一个驱动电动机就能够完成越障任务,改善了传统螺旋驱动式机器人越障能力不高的问题,同时也提高了对驱动电动机的使用效率。为了分析试验中发现的机器人保持架自转现象,对机器人进行运动分析,并由分析结果对相关部分进行改进。试验结果表明,该机器人能够在内径为190 mm和180 mm的管道中行进,并能够顺利通过两节管道间形成的同心台阶障碍,验证了自适应移动机构的行走能力。

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在主从式UUV 协作系统中,由于定位和导航的需要,要求尽快估计出从UUV 的航行参数,但通常所用的递推最小二乘(RLS)算法,其初始方位测量对滤波结果影响大且存在收敛速度慢、计算精度低的缺点,难以满足应用需求,而推广卡尔曼滤波(EKF)算法能较好地克服上述问题。在直角坐标系下(CEKF),方位信息与距离信息相互耦合导致初始振荡剧烈,改为混合坐标系(MEKF)后问题得到了极大的改善。最后,通过仿真及现场试验验证了此改进方法的有效性。

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根据主UUV观测系统测量的从UUV方位信息精度高、距离信息精度低的特点,将遗忘因子和位置权值构成的综合权值融入递推最小二乘算法(RLS)用于从UUV航行参数分析,避免采用EKF算法对观测噪声要求高的缺陷,克服数据饱和现象。同时对从UUV方位信息进行预处理以提高航行参数估计的收敛速度。仿真实验证明了方法的有效性。

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水下滑翔机器人是一种无外挂推进系统,仅依靠内置执行机构调整重心位置和净浮力来控制其自身运动的新型水下机器人,主要用于长时间、大范围的海洋环境监测,因此要求其具有低阻性和高稳定性.文章主要从水动力特性出发对水下滑翔机器人进行优化设计,包括主载体线型、升降翼和稳定翼的优化等,并对水动力优化设计的结构进行了定常滑翔运动和空间螺旋回转运动分析,这将为后期的控制系统设计提供参考.

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水下滑翔机器人是一种新型水下机器人,具有噪声低、航行距离远、续航时间长、成本低等特点。分析了水下滑翔机器人的驱动机理和运动实现,给出了水下滑翔机器人典型运动的仿真结果,并以正在设计的一水下滑翔机试验样机为研究对象,描述了样机的整体结构布局,详细研究了浮力调节机构、俯仰调节机构和横滚调节机构的实现方法,并就样机中各执行机构的设计实现进行了论述。

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AUV在长时间作业过程中需要浮出水面进行GPS定位,既浪费时间又浪费能源,因此仿照潜艇上的拖曳天线的形式,在AUV上采用了形状简单的GPS天线球,这种天线球的拖曳运动特性是本文的主要研究内容。 本文分析了这种天线球在静水环境下的拖曳运动情况,建立了拖曳系统的数学模型。其中对于缆绳采用了Ablow提出的有限差分模型,对于自由表面上的天线球,采用水动力系数法进行分析,对耦合的系统采用前向差分法进行求解。在此基础上编制程序进行仿真。 为了验证仿真结果,在拖曳水池进行了拖曳试验。在试验中通过改变拖曳速度和缆绳长度,得到了一系列的张力数据和天线球姿态。对试验数据和计算结果的比较表明,上面的数学模型在速度小于2节时能够模拟真实情况,反之则会出现较大的误差。经过查找,本文排除了试验误差和计算参数选取不当这两个可能的原因,最终认定是天线球的模型不够完善,因为它在自由表面上受到了兴波阻力的作用。 本文也对有限差分程序的结果和叶果洛夫给出的缆绳数据进行了比较,比较表明基于本文编写的缆绳分析程序是可靠的。在此基础上,本文把拖曳试验测量到的张力作为边界条件对实际工程进行了分析计算,指出目前缆绳长度14米的情况不能满足期望的10米拖曳深度;若要拖曳深度达到10米,需要加大天线球的浮力并增加缆绳长度,本文也给出了这种情况下的几组参数的具体值。

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采用模糊熵函数对图象象素分类作出整体最优分类评价,实现了区域分割.利用矩及其函数做为各区域的特征表达,构成以区域为基元的符号特征集并描述图象内容。根据立体图象对间的几何关系,解出各区域(基元)的相对三维坐标。与象索匹配相比较,它可以获得较高精度的三维信息和可描述的景物信息.通过获取不同时空的各区域(基元)三维信息,确定了它们的空间运动状态。联系这些状态,构造出景物中物体间的空间关系和近似模型,实现了对景物的3-D识别和描述。

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本文提出了一种新的活动图象分析法,该方法建立在高效的多级分辨率图象锥体算法的基础上,通过相关匹配估计图象序列连续帧间的位移,给出了计算机模拟结果。

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研究了空间飞行器编队中最具基础性的问题之一,即相对运动的解析表达及Hill方程的适用条件。通过建立相对运动的通解公式,针对不同性质的初值深入地分析了其相对运动轨迹的本质特征,并给出了Hill方程的适用条件。此外,文中还给出了一个新的编队设计简化公式。

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Singular perturbation theory of two-time scale expansions was developed both in inviscid and weak viscous fluids to investigate the motion of single surface standing wave in a liquid-filled circular cylindrical vessel, which is subject to a vertical periodical oscillation. Firstly, it is assumed that the fluid in the circular cylindrical vessel is inviscid, incompressible and the motion is irrotational, a nonlinear evolution equation of slowly varying complex amplitude, which incorporates cubic nonlinear term, external excitation and the influence of surface tension, was derived from solvability condition of high-order approximation. It shows that when forced frequency is low, the effect of surface tension on mode selection of surface wave is not important. However, when forced frequency is high, the influence of surface tension is significant, and can not be neglected. This proved that the surface tension has the function, which causes free surface returning to equilibrium location. Theoretical results much close to experimental results when the surface tension is considered. In fact, the damping will appear in actual physical system due to dissipation of viscosity of fluid. Based upon weakly viscous fluids assumption, the fluid field was divided into an outer potential flow region and an inner boundary layer region. A linear amplitude equation of slowly varying complex amplitude, which incorporates damping term and external excitation, was derived from linearized Navier-Stokes equation. The analytical expression of damping coefficient was determined and the relation between damping and other related parameters (such as viscosity, forced amplitude and depth of fluid) was presented. The nonlinear amplitude equation and a dispersion, which had been derived from the inviscid fluid approximation, were modified by adding linear damping. It was found that the modified results much reasonably close to experimental results. Moreover, the influence both of the surface tension and the weak viscosity on the mode formation was described by comparing theoretical and experimental results. The results show that when the forcing frequency is low, the viscosity of the fluid is prominent for the mode selection. However, when the forcing frequency is high, the surface tension of the fluid is prominent. Finally, instability of the surface wave is analyzed and properties of the solutions of the modified amplitude equation are determined together with phase-plane trajectories. A necessary condition of forming stable surface wave is obtained and unstable regions are illustrated. (c) 2005 Elsevier SAS. All rights reserved.

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It is demonstrated that when tension leg platform (TLP) moves with finite amplitude in waves, the inertia force, the drag force and the buoyancy acting on the platform are nonlinear functions of the response of TLP. The tensions of the tethers are also nonlinear functions of the displacement of TLP. Then the displacement, the velocity and the acceleration of TLP should be taken into account when loads are calculated. In addition, equations of motions should be set up on the instantaneous position. A theoretical model for analyzing the nonlinear behavior of a TLP with finite displacement is developed, in which multifold nonlinearities are taken into account, i.e., finite displacement, coupling of the six degrees of freedom, instantaneous position, instantaneous wet surface, free surface effects and viscous drag force. Based on the theoretical model, the comprehensive nonlinear differential equations are deduced. Then the nonlinear dynamic analysis of ISSC TLP in regular waves is performed in the time domain. The degenerative linear solution of the proposed nonlinear model is verified with existing published one. Furthermore, numerical results are presented, which illustrate that nonlinearities exert a significant influence on the dynamic responses of the TLP.

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To further investigate the mechanism of acoustic emission (AE) in the rock fracture experiment, moment tensor analysis was carried out. The AE sources characterized by crack sizes, orientations and fracture modes, are represented by a time-dependent momen

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This paper presents the Hill instability analysis of Tension Leg Platform (TLP) tether it, deep sea. The 2-D nonlinear beam model which is Undergoing Coupled axial and transverse vibrations, is applied. The governing equations are reduced to nonlinear Hill equation by use of the Galerkin's method and the modes superposition principle. The Hill instability charted Lip to large parameters is obtained. An important parameter M is defined and can he expressed as the functions of tether length, the platform surge and heave motion amplitudes. Some example studies are performed for various environmental conditions. The results demonstrate that the nonlinear coupling between the axial and transverse vibrations has a significant effect on the response of structure.. It needs to be considered for the accurate dynamic analysis of long TLP tether subjected to the combined platform surge and heave motions.

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By means of the matched asymptotic expansion method with one-time scale analysis we have shown that the inviscid geostrophic vortex solution represents our leading solution away from the vortex. Near the vortex there is a viscous core structure, with the length scale O(a). In the core the viscous stresses (or turbulent stresses) are important, the variations of the velocity and the equivalent height are finite and dependent of time. It also has been shown that the leading inner solutions of the core structure are the same for two different time scales of S/(ghoo)1/2 and S/a (ghoo)1/2. Within the accuracy of O(a) the velocity of a geostrophic vortex center is equal to the velocity of the local background flow, where the vortex is located, in the absence of the vortex. Some numerical examples demonstrate the contributions of these results.