三峡建库对长江中下游航道的影响及对策研究

三峡建库后，由于水沙条件的改变，长江中下游将发生长时间和长距离的河床冲刷，对整个长江中下游的航道条件产生举足轻重的影响。在对长江中下游航道进行现状分析的基础上，探讨三峡建库对中下游航道的影响并提出了相应的研究对策。     

三维数字城市的建设

提出了一种应用三维技术和虚拟现实交互技术来构建三维数字城市的设计思想和实施方案，探讨了具体实现三维数字城市系统而积累的实践经验，介绍了综合运用3DS MAX、AUTOCAD和CULT3D对“实例”进行制作的具体方法和步骤，并给出了部分制作结果。结果表明该系统获得了较好的实时浏览和交互浏览功能，且有良好的视觉效果。     

丹江口工程大坝加高后的几个水力学问题

依托1∶100水工模型试验成果,重点介绍了丹江口大坝加高后的几个水力学问题如泄流能力、坝面压力特性、河床局部冲刷、下游河道流速流态、泄洪对电厂及航运的影响等.研究显示:大坝加高后泄流能力可满足设计要求,坝下河床冲刷加重,挑距加远,设计洪水22 300 m3/s时坝下冲坑最低点高程为43.0 m,各级泄量冲坑上游坡均缓于临界坡,也略缓于初期工程同级流量冲坑的上游坡;坝下600 m以内为护岸工程重点防护段,岸边流速为5.8～9.8 m/s;泄洪对丹江口电厂影响较小,对自备电站不利影响较为显著;最大通航流量6 200 m3/s时下游引航道口门区流态复杂,水流较混乱.     

光总线在组合导航系统中的应用分析

航空电子系统和光通信发展到一定阶段，光总线将广泛应用于航空领域。在组合导航系统中，利用光总线进行通信可以极大地提高系统整体性能。本文介绍了光总线技术的发展及研究现状，重点分析了1394总线，提出了基于1394光总线的综合导航系统的网络结构及关键技术。     

DNS／GPS组合导航系统研究

本文阐述ＤＮＳ与ＧＰＳ组合导航的必要性、可行性及组合方法，给出了误差模型和卡尔曼滤波模型。选取观测量不同可有三种组合方式，通过模拟计算给出了相应曲线。当采用伪距及其变化率作为观测量时，其组合方式最佳，定位精度可达米级，航向精度可提高到０．２°。     

Self-calibration based on invariant view recognition: Dynamic approach to navigation

We extend a dynamic approach of behavior generation to the representation of spatial information. Two levels of dynamics integrate dead-reckoning, dominant far from home bases, and piloting, dominant near home bases. When the view-based piloting system recognizes a home base, visual place information recalibrates the dead-reckoning system, inverting the hierarchical ordering of the two dynamic levels by time scale inversion. Reference views taken at discrete home bases are recognized invariantly under rotation of views. This process yields compass information. Continuous translational information is obtained as a neural place representation built from view correlations with a scattered set of local views. This self-calibrating cognitive map couples into a dynamics of heading direction integrating the behaviors of obstacle avoidance and target acquisition. Targets can be designated in terms of the cognitive map. We demonstrate the dynamical model in simulation.     

Planetary exploration by robotic aerovehicles

Planetary aerobots are a new type of telerobotic science platform that can fly and navigate in a dynamic 3-dimensional atmospheric environment, thus enabling the global in situ exploration of planetary atmospheres and surfaces. Aerobots are enabled by a new concept in planetary balloon altitude control, developed at JPL, which employs reversible-fluid changes to permit repeated excursions in altitude. The essential physics and thermodynamics ofreversible-fluid altitude control have been demonstrated in a series of altitude-control experiments conducted in the Earth's atmosphere, which are described. Aerobot altitude-control technology will be important in the exploration of seven planets and satellites in our solar system. Three of these objects—Venus, Mars, and the Saturnian satellite Titan—have accessible solid surfaces and atmospheres dominated by the dense gases nitrogen or carbon dioxide. They will be explored with aerobots using helium or hydrogen as their primary means of buoyancy. The other four planets—Jupiter, Saturn, Uranus, and Neptune—have deep atmospheres that are predominantly hydrogen. It may be possible to explore these atmospheres with aerobots inflated with atmospheric gas that is then radiatively heated from the hotter gaseous depths below. To fulfill their potential, aerobots to explore the planets will need autonomous state estimators to guide their observations and provide information to the altitude-control systems. The techniques of acquiring these data remotely are outlined. Aerobots will also use on board altitude control and navigation systems to execute complex flight paths including descent to the surface and exploiting differential wind velocities to access different latitude belts. Approaches to control of these systems are examined. The application of aerobots to Venus exploration is explored in some detail: The most ambitious mission described, the Venus Flyer Robot (VFR), would have the capability to make repeated short excursions to the high-temperature surface environment of Venus to acquire data and then return to the Earth-like upper atmosphere to communicate and recool its electronic systems. Finally a Planetary Aerobot Testbed is discussed which will conduct Earth atmospheric flights to validate autonomous-state-estimator techniques and flight-path-control techniques needed for future planetary missions.     

LTN-72惯导设备在空间遥感器航空校飞中的应用

介绍了一种用于空间遥感器航空校飞的LTN-72惯导参数采集与传输装置。该装置能模拟星上数据管理系统(OBDH)传递包括校飞时间和全部LTN-72惯导参数在内的辅助数据,并具有输出检测信号和自检显示功能。装置经实际校飞使用,效果良好。     

Two years of operational use of Subpixel Automatic Navigation of AVHRR scheme: accuracy assessment and validation

Automated techniques for satellite imagery navigation and co-location are especially required for environmental monitoring activities intensively using satellite data. In this work are presented the results obtained after 2 years of operational use of the Subpixel Automatic Navigation of AVHRR (SANA) scheme. An automatic method for accuracy assessment of satellite navigation techniques, which permits a preliminary evaluation of their performances, dealing with a large collection of test images is also proposed. The navigation accuracy assessment, performed by using a selection of small islands as reference points, is discussed.Results achieved over more than 400 Advanced Very-High-Resolution Radiometer (AVHRR) scenes confirm that the SANA scheme is a very accurate one (computed mean navigation error is generally about one AVHRR pixel). Furthermore, because of its high processing speed, it can be considered a suitable tool for intensive satellite data processing in multitemporal analyses, especially required for environmental studies as well as for operational monitoring purposes.     

万顷沙西十三涌油轮码头模型试验研究

华隆公司拟在万顷沙西十二涌与十三涌之间兴十三涌３０００Ｔ级油轮港口码头。本文分析了该河段水文泥沙的特性、河道演变趋势及河段稳定性，通过物理模型试验研究及对航道、港池的回淤计算分析，预测工程建成后引起局部水流流态的变化，对水道泄洪、潮排、潮灌的影响，以及港池、航道建成后的泥沙淤积情况。