共查询到20条相似文献,搜索用时 343 毫秒
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超空泡水下航行器弹道控制技术是改进与优化超空泡航行器水下弹道的一种重要方式,其中对航行器尾翼的操纵是该技术的重要环节。在高速水洞实验室中进行了缩比模型通气超空泡的生成和尾翼力学特性实验研究,重点针对尾翼安装与否、不同后掠角和不同尾翼安装位置对模型超空泡形态和力学特性的影响进行了深入的分析。通过对比不同工况空泡的外形、阻力、侧向力和法向力矩,获得了尾翼后掠角以及安装位置对细长体超空泡尾部闭合和侧平面力学特性的影响规律,同时对实验结果进行了定性和定量分析。实验证实了尾翼后掠角和安装位置是影响超空泡尾部闭合与影响模型力学特征的重要因素,并提出了实现超空泡航行器尾翼的设计规律。 相似文献
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目前,国内外对于两栖航行器气动/水动特性的研究仍处于探索与发展阶段。结合鱼雷及水翼船的特点,提出一种通过改变外形实现水下、水面航行的新型两栖水翼航行器。基于LBM-LES方法对航行器水动特性进行数值仿真,得到航行器在水下、水面航行时的升力、阻力曲线。结果表明:在水下航行时,收缩水翼的航行器在较小的迎角范围内阻力较小,适合高速航行;在水面航行时,展开的水翼增大了航行器的升力、减小了阻力;通过改变外形航行器能够满足在水下、水面的航行要求,其外形设计及两栖航行性能还有较大的优化空间。 相似文献
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基于理性力学非线性几何场理论,建立了热弹性薄板等效速率形式的Karman方程,通过将热弹性薄板大挠度弯曲问题看成平板弯曲问题与平面大变形问题的耦合,在固定坐标系及拖带坐标系上推导出两组边界积分方程,从而建立起新的分析热弹性薄板大挠度弯曲的边界元法。算例表明本文方法理论可靠、精度高。 相似文献
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基于飞行仿真平台的相关坐标变换模型 总被引:2,自引:2,他引:0
李莹 《沈阳航空工业学院学报》2008,25(4)
飞行力学中相关的飞行器运动方程都是在地面坐标系中建立的,地面坐标系的前提假设"平面大地"与地球表面具有曲率不符,经纬度能真实反映飞行器的飞行情况,但不能直接运用于飞行器运动方程.针对以上情况,提出了能够运用于地面坐标与经纬度相互转换的模型.在飞行仿真平台上,由飞行器运动方程建立相关的飞行机动动作模型,再由提出的坐标变换模型将运动方程中的相关参数转换为经纬度.实验结果表明,坐标变换模型是合理的,具有实用性,能运用于相关的飞行仿真平台中. 相似文献
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临近空间高超声速飞行器天文导航系统综述 总被引:1,自引:1,他引:0
临近空间是航天与航空业务领域的结合部,具有重要的战略价值。高超声速飞行器是临近空间力量部署的重要载体,已逐渐进入应用部署阶段。临近空间高超声速飞行器的飞行环境和任务条件对导航系统提出了新的更高要求。在总结临近空间高超声速飞行器的导航技术研究进展的基础上,对天文导航技术的应用环境和条件进行了系统的分析和探讨,提出了5个重点研究方向,包括:星图采集效能、光学误差模型、视场观测机理、姿态更新速率、小型化模块化工程化等。研究结果可为临近空间高超声速飞行器天文导航系统的设计提供参考。 相似文献
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The problems are considered of a modelling research of navigation features and improvement of the navigating filters algorithms used in the navigating devices of ground mobile vehicles (MV). It is supposed that the methods and approaches known as real time kinematic (RTK) are incorporated in a basis of researched navigating devices and algorithms. Thus, the measurements from satellite navigating systems such as GLONASS/GPS, and also the measurements from other traditional measuring means (tactile sensors, steering wheel angle and/or inertial measuring instruments) are used in the navigating device of the MV. In the present report we solve the problems and describe the methods of a modeling research of the features of functional units algorithms of the MV navigating processor with account of a satellite navigation set integration with other measuring instruments. The improvement of these devices interaction is made by means of the computer complex "AutoMobil," allowing us to simulate the certain conditions of these navigating tools operation. The imitation computer complex "AutoMobil" for researches of the MV navigation is developed within the frameworks of a programming environment "Delphi-7". 相似文献
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Safe, reliable, and low cost space-based navigation is being provided with embedded INS/GPS systems such as the space integrated GPS/INS (SIGI). The SIGI is being used for various space vehicle applications such as launch vehicles, orbital vehicles, and re-entry vehicles. This paper describes current space vehicle navigation capabilities. The SIGI is being enhanced to provide additions to these existing capabilities with such items as higher processing and a commercial-off-the-shelf operating system. This will allow hosting of various software applications such as advanced navigation functions, flight control, guidance and vehicle management algorithms. The SIGI can host redundancy management functions by incorporating a cross channel data link card (CCDL) using a high speed firewire bus. The SIGI can then be used as a redundancy management platform which has application to current space vehicle avionics topologies incorporating distributed processing architectures 相似文献
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Jianping Yuan Jianjun Luo Xiaomu Dou Qun Fang 《Aerospace and Electronic Systems Magazine, IEEE》1998,13(12):25-28
A type of multi-spacecraft system with kinematical restraint but no structural restraint and force action is considered. Both the absolute and relative navigation information is required for this multi-spacecraft system, but the relative information is more critical and the accuracy requirements for relative information will be much higher than those for the absolute information. In this paper, the Global Positioning System (GPS)/Differential GPS (DGPS) are introduced and used for relative navigation. Relative motion of space vehicles is modeled. Relative position, relative velocity and relative attitude are represented and solved by GPS/DGPS measurements. Using a type of commercial GPS receiver onboard spacecraft and relative differential GPS technique, the relative navigation of space vehicles can be implemented in real-time 相似文献
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以电磁波三维空间结构向量为参照的飞行器姿态/航向测量研究,可弥补空间参照物缺乏,丰富空间飞行器姿态/航向测量工具。本文根据各缺损电磁矢量传感器姿态位置与接收信号之间的变化规律,建立飞行器载电磁矢量传感器阵列导向矢量。根据协同导航的多个信号空间谱和最大化,实现平台姿态/航向测量。飞行器多位置的多个传感器共同测量姿态可避免遮挡,获得更高姿态精度的同时拓展了系统的适用领域。接收电磁信息完备状态下,不需导航信号,测绘平稳的杂波就能作为姿态基准。仿真试验验证了姿态估计的有效性。 相似文献
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《IEEE transactions on aerospace and electronic systems》1988,24(5):474-519
An examination is made of old and new navigation technology that considers most factors affecting this technology, including cost, accuracy, autonomy, time-delay, global coverage, and the human interface. The author reviews cartography and the navigation of land, ship, air, and space vehicles, concluding with a forecast of navigation in the twenty-first century. An extensive annotated bibliography is included 相似文献