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121.
122.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2020,65(10):2360-2371
The Global Positioning System (GPS) variometric approach has emerged as an attractive alternative to traditional well-developed positioning techniques including relative positioning and precise point positioning. Previous studies have demonstrated the capability of the variometric approach to retrieve coseismic displacements at centimeter-level precision, in a real-time manner using only readily available broadcast ephemeris. This study presents the first results comparing the performance of the variometric approach by using a variety of precise satellite orbit and clock products. Totally six kinds of products are included in our evaluation, namely the broadcast, IGS (International GNSS Service) ultra-rapid (predicted), ultra-rapid (observed), rapid, final (30-s clock) and CODE (Center for Orbit Determination in Europe) final (5-s clock) products. Static and dynamic experiments are conducted using 1-Hz GPS data covering a relatively large area in China during the 2008 Wenchuan MW 7.9 earthquake. After removing the linear trend, the displacements using broadcast, ultra-rapid (predicted), ultra-rapid (observed) and rapid products reach nearly equivalent precisions at centimeter level. By using final and CODE final products, the precision of displacements can be significantly improved from 1.9–2.0 cm to 0.4–0.7 cm horizontally, and from 6.0–6.2 cm to 1.0–1.7 cm vertically for the dynamic experiments. The displacements using the CODE final products achieve the best precision, improved by more than 40% compared to those using the IGS final products. With the availability of IGS high-rate real-time precise products, this approach is promising to capture coseismic displacements more precisely in real time, which is crucial for earthquake and tsunami early warning. 相似文献
123.
动力下降点确定是实施月面软着陆的重要环节,是多系统间复杂迭代的过程,涉及轨道设计、制导律设计、着陆目标的采样区确定、着陆及起飞安全分析。其设计结果直接影响了最终着陆点的位置和着陆过程的着陆安全,也间接影响采样安全和采样工程目标的实现结果。针对嫦娥五号在实施月面软着陆前确定动力下降点的任务需求,提出了通过多次轨道控制与最优标称制导轨迹搜索联合控制策略的动力下降点确定方法。首先,根据月面无人自主采样返回任务设计总结了动力下降点确定原理和约束条件;然后,详细论述了月面无人自主采样返回任务软着陆过程动力下降点确定方法;最后,通过嫦娥五号在着陆前主要的几次轨控实施结果分析了其对动力下降点的影响,同时综合了着陆区地形分析及着陆、起飞安全性分析,对动力下降点进行确定并根据最终在轨飞行结果进行验证。验证结果表明,基于“逐次逼近寻优方法”的月面软着陆环节动力下降点的确定方法有效,可以为后续地外天体软着陆等任务提供参考和借鉴。 相似文献
124.
125.
未来的深空通信需要一个鲁棒的、有效与可靠的文件传输协议,在研究CCSDS提出的CFDP协议基础上,针对延迟NAK模式提出了一种新的分析方法。在保证吞吐量的前提下,对ARQ定时器优化设置,导出了平均文件传输时间的理论表达式。在单跳直连链路中,对不同条件下的平均文件传输时间进行了仿真与数值分析。仿真结果表明平均文件传输时间与PDU错误概率、PDU数目及单向传播时间等有密切关系。随机仿真与理论分析具有很好的一致性。 相似文献
126.
Dmitri Nikolaevich Severov Valentina Pshennikov Alexsandr Vasilievich Remeslo 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
Fronts and thermohaline structure of the Brazil–Malvinas Confluence System (BMCS) are studied from climatic data, “Marathon Exp. Leg.8, 1984” data, and Sea surface temperature (SST) data base “ds277-Reynolds” (1981–2000). The South Atlantic Central Water (SACW) is divided in two main types: tropical (TW) and subtropical water (ST). Water masses, Fronts, Inter-Frontal and Frontal Zones are analysed and classified: (a) the water masses: Tropical Low-Salinity Water, Tropical Surface Water, Tropical Tropospheric Water, Subtropical Low-Salinity Water, Subtropical Surface Water, Subtropical Tropospheric Water. T,S characteristics of intermediate, deep and bottom water defined by different authors are confirmed and completed; (b) the Inter-Frontal Zones: Tropical/Brazil Current Zone, Subtropical Zone and Subantarctic Zone; (c) the Frontal Zones: Subtropical, Subantarctic and Polar, and (d) the Fronts: Subtropical Front of the Brazil Current, Principal Subtropical Front, North Subtropical Front, Subtropical Surface Front, South Subtropical Front, Subantarctic Surface Front, Subantarctic Front and Polar Front. Several stable T–S relationships are found below the friction layer and at the Fronts. The maximum gradient of the oceanographic characteristics occurs at the Brazil Current Front, which can be any of the subtropical Fronts, depending on season. Minimum mean depth of the pycnocline coincides with the Fronts of the BMCS, indicating the paths of low-salinity shelf waters into the open ocean. In the work it is shown how to recover the horizontal and vertical thermohaline structure of waters from satellite data RSMAS SST. 相似文献
127.
介绍一个多通道多采样率的数据采集系统。该系统输入64个模拟量均要转换成数字信号,数据采集卡为基于VXI总线的E1413,多通道之间的变采样率通过特殊的采样列表实现。文中给出了硬件组成、软件设计和测试结果。该系统已用于对飞机燃油试验台的测控。 相似文献
128.
首先将标准有限元程序与改进的均值法相结合,对某型飞机翼身连接接头处的刚度可靠性进行分析,结果表明,在所给载荷和允许应变情况下,该接头结构在外载变异系数为0.15,弹性模量和剪切模量为0.05时,仍具有较高的可靠度。然后,又将标准有限元分析程序与响应面法结合,在假设接头的响应极限状态方程为一不包括交叉项的二次多项式的基础上,利用有限元分析确定响应极限状态方程,通过迭代运算,保证响应极限状态方程在最有可能失效点处与接头结构真实的隐式极限状态方程有很好的近似程度。2种方法的计算结果具有较好的一致性。最后,基于弹塑性应变分析,给出了在大过载情况下的低周疲劳寿命可靠性分析结果,得到了在给定寿命要求下,结构可靠度随寿命变异系数变化的曲线,并给出了在要求寿命可靠度情况下,可靠寿命随寿命变异系数的变化曲线,从而,为该型飞机的设计定型提供了有力的依据和方法。 相似文献
129.
NASA深空网(DSN)的现状及发展趋势 总被引:10,自引:0,他引:10
详细介绍了美国深空网的发展过程、目前的状况以及未来的主要发展计划。 相似文献
130.
C. M. Lisse M. F. A’Hearn T. L. Farnham O. Groussin K. J. Meech U. Fink D. G. Schleicher 《Space Science Reviews》2005,117(1-2):161-192
As comet 9P/Tempel 1 approaches the Sun in 2004–2005, a temporary atmosphere, or “coma,” will form, composed of molecules
and dust expelled from the nucleus as its component icy volatiles sublimate. Driven mainly by water ice sublimation at surface
temperatures T > 200 K, this coma is a gravitationally unbound atmosphere in free adiabatic expansion. Near the nucleus (≤ 102 km), it is in collisional equilibrium, at larger distances (≥104 km) it is in free molecular flow. Ultimately the coma components are swept into the comet’s plasma and dust tails or simply
dissipate into interplanetary space. Clues to the nature of the cometary nucleus are contained in the chemistry and physics
of the coma, as well as with its variability with time, orbital position, and heliocentric distance.
The DI instrument payload includes CCD cameras with broadband filters covering the optical spectrum, allowing for sensitive
measurement of dust in the comet’s coma, and a number of narrowband filters for studying the spatial distribution of several
gas species. DI also carries the first near-infrared spectrometer to a comet flyby since the VEGA mission to Halley in 1986.
This spectrograph will allow detection of gas emission lines from the coma in unprecedented detail. Here we discuss the current
state of understanding of the 9P/Tempel 1 coma, our expectations for the measurements DI will obtain, and the predicted hazards
that the coma presents for the spacecraft.
An erratum to this article is available at . 相似文献