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891.
最差用户位置算法研究与仿真分析 总被引:2,自引:1,他引:2
在计算Galileo卫星导航系统空间信号误差(SISE)、空间信号精度(SI-SA)和空间信号监测精度(SISMA)时需要用到的一个关键参数——最差用户位置(WUL)。WUL表示空间信号的轨道误差在卫星覆盖域内所导致的伪距误差最大的位置,WUL的确定可以帮助系统向用户提供正确可靠的SISA、SISMA和完好性标志(IF)等完好性信息,对提高系统的可靠性和可用性具有非常重要的意义。WUL的算法主要有两种:临界圆法和网格搜索法。详细介绍两种算法的基本原理与计算流程,比较两种算法的结果,并基于全球和区域完好性监测的概念对二者进行分析评价。 相似文献
892.
新型升力再入飞船返回舱气动外形选型研究 总被引:2,自引:0,他引:2
未来低成本天地往返运输系统的气动外形设计的总体要求是升阻比高、机动性强、稳定性好、过载低、空间大、可重复使用等。结合国内技术水平和国外经验教训,提出了我国未来新型升力再入飞船返回舱的总体气动需求,采用平面斜切二次曲线构造截面的模线设计方法,设计了四种满足长度、截面尺寸和容积等总体需求的返回舱布局方案。利用基于牛顿理论的气动力工程方法对气动特性进行预测,利用气动力与六自由度弹道的耦合计算研究返回舱无控再入飞行特性。研究表明,所设计的返回舱外形高超声速稳定配平升阻比大于0.9,阻力系数大于0.5,法向过载低于2.5,具有较好的静动稳定性,具备可部分重复使用的潜力。 相似文献
893.
894.
长期以来,拉萨机场规定进出港航空器在泽当以西严禁对头起降(09号跑道起飞,27号跑道落地),在正常的情况下,这样做有其必要性与合理性:
1.拉萨机场进近航路周围地形复杂,山高均在5000米左右,进离港航空器沿雅鲁藏布江河谷飞行,没有回旋避让的余地; 相似文献
895.
897.
898.
The deformation work rate can be expressed by the time rate of pair functional potentials which describe the energy of mate-rials in terms of atomic bonds and atom embedding interactions. According to Cauchy-Born rule, the relations between the microscopic deformations of atomic bonds and electron gas and macroscopic deformation are established. Further, atomic bonds are grouped according to their directions, and atomic bonds in the same direction are simplified as a spring-bundle component. Atom embedding interactions in unit reference volume are simplified as a cubage component. Consequently, a material model composed of spring-bundle components and a cubage component is established. Since the essence of damage is the decrease and loss of atomic bonding forces, the damage effect can be reflected by the response functions of these two kinds of compo-nents. Formulating the mechanical responses of two kinds of components, the corresponding elasto-damage constitutive equa-tions are derived. Considering that slip is the main plastic deformation mechanism of polycrystalline metals, the slip systems of crystal are extended to polycrystalline, and the slip components are proposed to describe the plastic deformation. Based on the decomposition of deformation gradient and combining the plastic response with the elasto-damage one, the elasto-plastic dam-age constitutive equations are derived. As a result, a material model formulated with spring-bundle components, a cubage component and slip components is established. Different from phenomenological constitutive theories, the mechanical property of materials depends on the property of components rather than that directly obtained on the representative volume element. The effect of finite deformation is taken into account in this model. Parameter calibration procedure and the basic characteris-tics of this model are discussed. 相似文献
899.
900.
Zhong Lingwei Liu Yu Li Juan Gu Zuo Jiang Haocheng Wang Haixing Tang Haibin 《中国航空学报》2010,23(1):15-21
Charge exchange(CEX) ions could inflict severe damages on the ion thruster optical system. This article is aimed at investigating the characteristics of the CEX ions and their influences upon the optical system by means of particle-in- cell(PIC) ion simulation and Monte Carlo collision(MCC) methods. The results from numerical simulation indicate that despite the fact that CEX ions appear in the entire beamlet region near the ion optical system, the ones that present themselves downstream of the accelerator grid have good reason for attracting more attention. As their trajectories are significantly affected by the local electric field, a great number of CEX ions are accelerated toward grids resulting in sputtering erosion. When the influences of the CEX ions are considered in the numerical simulation, there could hardly be observed augments in the screen grid current, but the accelerator grid current increases from zero to 1. 4% of the beamlet current. It can be understood from the numerical simulation that the CEX ions formed in the region far downstream of the accelerator grid should be blamed for the erosion on the downstream surface of the accelerator grid. 相似文献