全文获取类型
收费全文 | 5129篇 |
免费 | 649篇 |
国内免费 | 484篇 |
专业分类
航空 | 2673篇 |
航天技术 | 1452篇 |
综合类 | 435篇 |
航天 | 1702篇 |
出版年
2024年 | 15篇 |
2023年 | 47篇 |
2022年 | 108篇 |
2021年 | 165篇 |
2020年 | 129篇 |
2019年 | 112篇 |
2018年 | 182篇 |
2017年 | 181篇 |
2016年 | 171篇 |
2015年 | 170篇 |
2014年 | 245篇 |
2013年 | 233篇 |
2012年 | 252篇 |
2011年 | 311篇 |
2010年 | 330篇 |
2009年 | 374篇 |
2008年 | 329篇 |
2007年 | 259篇 |
2006年 | 195篇 |
2005年 | 204篇 |
2004年 | 147篇 |
2003年 | 182篇 |
2002年 | 196篇 |
2001年 | 186篇 |
2000年 | 137篇 |
1999年 | 140篇 |
1998年 | 109篇 |
1997年 | 111篇 |
1996年 | 112篇 |
1995年 | 108篇 |
1994年 | 86篇 |
1993年 | 55篇 |
1992年 | 73篇 |
1991年 | 43篇 |
1990年 | 38篇 |
1989年 | 51篇 |
1988年 | 31篇 |
1987年 | 26篇 |
1986年 | 30篇 |
1985年 | 77篇 |
1984年 | 41篇 |
1983年 | 27篇 |
1982年 | 40篇 |
1981年 | 76篇 |
1980年 | 18篇 |
1978年 | 10篇 |
1977年 | 14篇 |
1976年 | 11篇 |
1975年 | 14篇 |
1974年 | 17篇 |
排序方式: 共有6262条查询结果,搜索用时 511 毫秒
801.
M. Tátrallyay G. Erdős A. Balogh I. Dandouras 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(10):1537-1544
Two orbits were selected in January–February 2006 when the separation between the Cluster spacecraft was large and mirror type magnetic field fluctuations were observed by all spacecraft in different regions of the terrestrial magnetosheath. Minimum variance analysis was applied to find the mirror type fluctuations, and the amplitude of the fluctuations was determined individually. Mirror mode structures are moving along the streamlines frozen in the plasma. A model was developed for the calculation of plasma flowtime from the bow shock to the observation point. The growth rate of the field strength perturbations was estimated by comparing the amplitudes of fluctuations observed simultaneously at distant locations (∼10,000 km) based on the assumption that δB ∼ exp(γt). The obtained growth rate values were about an order of magnitude smaller than those provided by linear models and they decreased in the inner regions of the magnetosheath, indicating some saturation in the growth of the waves when proceeding towards the magnetopause. The results of these two case studies suggest that mirror type fluctuations originate from the compression region downstream of the quasi-perpendicular bow shock, and the growth of the fluctuations cannot be described by linear approximations. 相似文献
802.
Chikovani V.V. Yatsenko Yu.A. Barabashov A.S. Marusyk P.I. Umakhanov E.O. Taturin V.N. 《Aerospace and Electronic Systems Magazine, IEEE》2009,24(5):40-43
Metallic resonator Q-factor is very sensitive to the resonator's material, its thermal and chemical treatment, design, and environment; i.e., pressure and temperature. In order to obtain higher accuracy for CVG it is necessary to use resonator evacuation. Resonator mass plays a very important role in sensitivity to angle rate, in stability of vibration, in response to environmental condition changes, and also to external vibration and shock resistance. tnnalabs Holding Inc. uses a cylindrical resonator with increased rim thickness of up to 2 mmn and more. This concerns resonator material and design parameters selection, material thermal treatment to increase resonator Q-factor, and improved control algorithms in order to increase metallic CVG accuracy. As a result, CVG bias instability of 0.025 degth and random walk of 0.008 degvh for the resonator diameter 43 mmn, and 0.2 deg/h for the resonator diameter 25 mm were obtained. Future opportunities for Innalabs CVG is also discussed herein. Test results are presented for CVG43 and CVG25. Three-axis CVG unit under control of one DSP "Sharc" and IMU parameters are forecasted. 相似文献
803.
P. P. Pavlov R. S. Litvinenko M. N. Mubarakhin I. O. Yushin V. M. Nigmatullin 《Russian Aeronautics (Iz VUZ)》2008,51(2):198-204
A technique for selecting a rational variant of a multifunctional aircraft system using the analytic hierarchy process is proposed and a solution of a practical problem is presented. 相似文献
804.
T.P. Dachev B. Tomov Yu. Matviichuk Pl. Dimitrov N. Bankov 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2009
The paper presents observation of relativistic electrons. Data are collected by the Radiation Risk Radiometer-Dosimeters (R3D) B2/B3 modifications during the flights of Foton M2/M3 satellites in 2005 and 2007 as well as by the R3DE instrument at the European Technology Exposure Facility (EuTEF) on the Columbus External Payload Adaptor at the International Space Station (ISS) in the period February 20 – April 28, 2008. On the Foton M2/M3 satellites relativistic electrons are observed more frequently than on the ISS because of higher (62.8°) inclination of the orbit. At both Foton satellites the usual duration of the observations are a few minutes long. On the ISS the duration usually is about 1 min or less. The places of observations of high doses due to relativistic electrons are distributed mainly at latitudes above 50° geographic latitude in both hemispheres on Foton M2/M3 satellites. A very high maximum is found in the southern hemisphere at longitudinal range 0°–60°E. At the ISS the maximums are observed between 45° and 52° geographic latitude in both hemispheres mainly at longitudes equatorward from the magnetic poles. The measured absolute maximums of dose rates generated by relativistic electrons are found to be as follows: 304 μGy h−1 behind 1.75 g cm−2 shielding at Foton M2, 2314 μGy h−1 behind 0.71 g cm−2 shielding at Foton M3 and 19,195 μGy h−1 (Flux is 8363 cm−2 s−1) behind les than 0.4 g cm−2 shielding at ISS. 相似文献
805.
806.
807.
The results of modeling the dynamics of the Space Radiotelescope are presented. The results of ground-based vibration-dynamic tests are used to validate the calculation models and estimate the damping levels. The dynamic distortions of the reflecting surface caused by the operation of the pointing mechanism of the high-gain antenna are estimated. 相似文献
808.
D. Abplanalp P. Wurz L. Huber I. Leya E. Kopp U. Rohner M. Wieser L. Kalla S. Barabash 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2009,44(7):870-878
The Polar Balloon Atmospheric Composition Experiment (P-BACE) is a new generation of neutral gas mass spectrometer based on the time-of-flight principle. P-BACE is the scientific experiment on the Mars Environment Analog Platform (MEAP) flown successfully on a balloon mission in summer 2008. The MEAP mission was flown with a 334,000 m3 helium balloon in the stratosphere on a semicircular trajectory from northern Sweden around the North Pole to Canada using the summer northern hemispheric wind current. The atmospheric conditions at an atmospheric altitude of 35–40 km are remarkably similar to those on the surface of Mars and thus the balloon mission was an ideal testbed for our mass spectrometer P-BACE. Originally this instrument was designed for in situ measurements of the chemical composition of the Martian atmosphere.P-BACE has a unique mass range from 0 to 1000 amu/q with a mass resolution m/Δm (FWHM) > 1000, and the dynamic range is at least six orders of magnitude. During this experiment, the acquisition of one mass spectrum is a sum of 65,535 single spectra, recorded in a time frame of 66 s.The balloon mission lasted 5 days and had successfully demonstrated the functionality of the P-BACE instrument during flight conditions. We had recorded more than 4500 mass spectra. With little modifications, P-BACE can be used on a planetary mission for Mars, but for example also for Venus or Mercury, if placed on a satellite. 相似文献
809.
D. S. Ivanov N. A. Ivlev S. O. Karpenko M. Yu. Ovchinnikov D. S. Roldugin S. S. Tkachev 《Cosmic Research》2014,52(3):205-215
The attitude control system of the Chibis-M microsatellite is described. Results of flight experiments on damping the initial angular velocity (made using magnetorquers) are considered, as well as stabilization in the orbital referece frame, and orientation of solar arrays toward the Sun using reaction wheels. The operation of algorithms of satellite attitude determination on sunlit and shadow segments of the orbit is also under study. The general logic of operation of the attitude control system in automatic mode is presented and discussed. 相似文献
810.
I M Shirobokova N S Pechurkin 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2003,31(7):1737-1741
A mathematical model was used to investigate the effect of cannibalism intensity on the net primary production and the dynamics of trophic links in an aquatic ecosystem characterized by cannibalism at the upper trophic level. A mathematical model of an aquatic ecosystem has been constructed, with the following principal trophic links: limiting nutrient concentration, producers (phytoplankton), nonpredatory and predatory zooplankton. The model takes into account the age structure of the predator and includes two age groups (the young and adults). The adult predators are cannibals feeding on both nonpredatory zooplankton and their own young, which consume phytoplankton. It has been found that when cannibalism intensity increases above a certain level, the concentrations of both adults and the young of the predators decrease. At the same time, the concentrations of the nonpredatory zooplankton and of nutrients increase, while the biomass of producers decreases. When the cannibalism intensity is low, the net primary production of the system increases to a certain level correlated with the increase in cannibalism intensity and drops sharply when the level of consumption of young is high. There is an optimal intensity of cannibalism, at which the productivity in the photosynthesis link is maximal. 相似文献