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961.
余德义 《南京航空航天大学学报》1995,27(2):280-283
50年代末,南京航天航天大学就开始研究仿真技术工作,并研制成功包括三自由度液压飞行模拟转台在内的若干专用模拟器。在这套仿真设备上,圆地完成了多种型号无人驾驶飞机、导弹、舰船控制系统地面仿真试验。本文简要地介绍这套设备的技术性能,以及系统仿真在飞行控制系统研制过程中不同阶段的应用效果。 相似文献
962.
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964.
A mode of motion of a satellite with respect to its center of mass is studied, which is called the biaxial rotation in the orbit plane. In this mode of rotation, an elongated and nearly dynamically symmetric satellite rotates around the longitudinal axis, which, in turn, rotates around the normal to the plane of an orbit; the angular velocity of rotation around the longitudinal axis is several times larger than the orbital angular velocity, deviations of this axis from the orbit plane are small. Such a rotation is convenient in the case when it is required to secure a sufficiently uniform illumination of the satellite's surface by the Sun at a comparatively small angular velocity of the satellite. The investigation consists of the numerical integration of equations of the satellite's motion, which take into account gravitational and restoring aerodynamic moments, as well as the evolution of the orbit. At high orbits, the mode of the biaxial rotation is conserved for an appreciable length of time, and at low orbits it is destroyed due to the impact of the aerodynamic moment. The orbit altitudes and the method of constructing the initial conditions of motion that guarantee a sufficiently prolonged period of existence of this mode are specified. 相似文献
965.
本文提出了铅化合物催化双基推进剂燃烧的反应历程。充分说明这类化合物是最终通过提高燃烧表面处嘶嘶区温度梯度提高燃速的。本文还提出了“铅化合物有通过增加燃烧表面上碳质物量增加燃速的一面,还有通过减少碳质物抑制燃速增加的一面”这一新的论点及抑制碳质物增加的反应并阐明了压力对这种抑制能力的影响。最后根据本文提出的作用机理及传热原理圆满解释了超速、平平和/或麦撒效应。 相似文献
966.
In this paper we continue the analysis of the influence of solar and interplanetary events on magnetic storms of the Earth that was started in [9, 10]. Different experimental results on solar-terrestrial physics are analyzed in the study and the effects are determined that arise due to differences in the methods used to analyze the data. The classifications of magnetic storms by the K
p and D
st indices, the solar flare classifications by optical and X-ray observations, and the classifications of different geoeffective interplanetary events are compared and discussed. It is demonstrated that quantitative estimations of the relationships between two types of events often depend on the direction in which the events are compared. In particular, it was demonstrated that the geoeffectiveness of halo CMEs (that is, the percentage of Earth-directed coronal mass ejections that result in geomagnetic storms) is 40–50%. Higher values given in some papers were obtained by another method, in which they were defined as the probability of finding candidates for a source of geomagnetic storms among CMEs, and, strictly speaking, these values are not true estimates of the geoeffectiveness. The latter results are also in contrast with the results of the two-stage tracing of the events: first a storm—an interplanetary disturbance, and then an interplanetary disturbance—a CME. 相似文献
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968.
固体火箭发动机性能精度分析 总被引:1,自引:2,他引:1
根据固体火箭发动机内弹道计算模型,提出了内弹道计算中的独立随机变量,建立了随机变量的概率统计模型,确定了参数的分布规律,并用Monte—Carlo法进行了内弹道模拟计算。最后对发动机性能的均值。和标准差σ进行了分析和实验验证,得出了计算方法可行,数据可信的结论。 相似文献
969.
E. V. Babkin M. Yu. Belyaev N. I. Efimov V. V. Sazonov V. M. Stazhkov 《Cosmic Research》2001,39(1):23-37
The results of determining the rotational motion of the Mir orbital station are presented for four long segments of its unmanned uncontrolled flight in 1999–2000. The determination was carried out using the data of onboard measurements of the Earth's magnetic field intensity. These data, taken for a time interval of several hours, were jointly processed by the least squares method with the help of integration of the equations of station motion relative to its center of mass. As a result of this processing, the initial conditions of motion and the parameters of the mathematical model used were evaluated. The technique of processing is verified using the telemetry data on angular velocity of the station and its attitude parameters. Two types of motion were applied on the investigated segments. One of them (three segments) presents a rotation around the axis of the minimum moment of inertia. This axis executes small oscillations with respect to a normal to the orbit plane. Such a motion was used for the first time on domestic manned orbital complexes. The second type of motion begins with a biaxial rotation which, in a few weeks, goes over into a motion very similar to the rotation around the normal to the orbit plane, but around the axis of the maximum moment of inertia. 相似文献
970.