全文获取类型
收费全文 | 2528篇 |
免费 | 9篇 |
国内免费 | 5篇 |
专业分类
航空 | 1187篇 |
航天技术 | 917篇 |
综合类 | 10篇 |
航天 | 428篇 |
出版年
2021年 | 18篇 |
2019年 | 16篇 |
2018年 | 59篇 |
2017年 | 36篇 |
2016年 | 39篇 |
2015年 | 12篇 |
2014年 | 57篇 |
2013年 | 89篇 |
2012年 | 55篇 |
2011年 | 85篇 |
2010年 | 71篇 |
2009年 | 118篇 |
2008年 | 139篇 |
2007年 | 58篇 |
2006年 | 63篇 |
2005年 | 64篇 |
2004年 | 64篇 |
2003年 | 85篇 |
2002年 | 43篇 |
2001年 | 92篇 |
2000年 | 48篇 |
1999年 | 65篇 |
1998年 | 69篇 |
1997年 | 66篇 |
1996年 | 64篇 |
1995年 | 87篇 |
1994年 | 86篇 |
1993年 | 41篇 |
1992年 | 50篇 |
1991年 | 15篇 |
1990年 | 24篇 |
1989年 | 51篇 |
1988年 | 32篇 |
1987年 | 20篇 |
1986年 | 29篇 |
1985年 | 74篇 |
1984年 | 70篇 |
1983年 | 42篇 |
1982年 | 69篇 |
1981年 | 67篇 |
1980年 | 17篇 |
1979年 | 10篇 |
1978年 | 31篇 |
1977年 | 12篇 |
1975年 | 24篇 |
1974年 | 16篇 |
1973年 | 16篇 |
1972年 | 16篇 |
1970年 | 9篇 |
1969年 | 12篇 |
排序方式: 共有2542条查询结果,搜索用时 0 毫秒
991.
Krishnamoorthy B.M. Krishnamurthy M.R. 《IEEE transactions on aerospace and electronic systems》1982,(1):58-75
The asynchronous performance of a polyphase reluctance machine with rotor provided with axial slits is investigated for the first time on the basis of conductor boundary treated as a flux line. Theoretical and experimental investigations are presented for rotors with 1) many values of pole arc/pole pitch ratio, 2) varying slot depths, 3) slots on either pole faces or slot portions or both of them, and 4) with and without terminating end rings. Their comparison with predictions leads to interesting conclusions. 相似文献
992.
S. B. Colegrove S. J. Davey B. Cheung 《IEEE transactions on aerospace and electronic systems》2006,42(4):1492-1496
A typical tracking algorithm takes its input from a peak detector or plot extractor. This process reduces the sensor image data to point measurements and reduces the volume of data that the tracker must process. However, useful information can be lost. This paper shows how the clutter of a peak can be a useful feature for discriminating false alarms and valid detections. The benefit obtained by using this feature is quantified through false track rate on recorded sensor data. On recorded data with difficult clutter conditions, approximately sixty percent of false tracks are rejected by exploiting peak curvature 相似文献
993.
Lohr D. A. Zanetti L. J. Anderson B. J. Potemra T. A. Hayes J. R. Gold R. E. Henshaw R. M. Mobley F. F. Holland D. B. Acuña M. H. Scheifele J. L. 《Space Science Reviews》1997,82(1-2):255-281
The primary objective of the investigation is the search for a body-wide magnetic field of the near Earth asteroid Eros. The Near Earth Asteroid Rendezvous (NEAR) 3-axis fluxgate magnetometer includes a sensor mounted on the high-gain antenna feed structure. The NEAR Magnetic Facility Instrument (MFI) is a joint hardware effort between GSFC and APL. The design and magnetics approach achieved by the NEAR MFI effort entailed low-cost, up-front attention to engineering solutions which did not impact the schedule. The goal of the magnetometer is reliable magnetic field measurements within 5 nT, which necessitates the use of an extensive spacecraft magnetic interference model but is achievable with the full year's orbital data set. Such a goal has been shown viable with recent in-flight calibration data and comparisons to the WIND magnetometer data. The NEAR MFI effort has succeeded in providing magnetic field measurements for the first flight in NASA's Discovery line. 相似文献
994.
Gai E.G. Adams M.B. Walker B.K. 《IEEE transactions on aerospace and electronic systems》1976,(6):744-755
A systematic approach for the determination of failure thresholds for hybrid navigation systems is described. Cost functions which reflect the importance assigned to the consequences of false and missed alarms are minimized. The false alarm probability is obtained as a function of the threshold magnitude by observing the statistical behavior of the instrument outputs in the normal operating mode. The missed alarm probability is obtained by determining the sensitivity of navigation error performance to instrument error sources. Two cost functions are considered. To illustrate this method, failure detection and identification (FDI) thresholds are determined for the Space Shuttle Approach and Landing Test flight. 相似文献
995.
Numerical results obtained based on the equations for the general theory of physically orthotropic shells are presented. These results illustrate the influence of anisotropy for mechanical and physical characteristics of material on stressed state. 相似文献
996.
Hawkins S. Edward Darlington E. Hugo Murchie Scott L. Peacock Keith Harris Terry J. Hersman Christopher B. Elko Michael J. Prendergast Daniel T. Ballard Benjamin W. Gold Robert E. Veverka Joseph Robinson Mark S. 《Space Science Reviews》1997,82(1-2):31-100
A multispectral imager has been developed for a rendezvous mission with the near-Earth asteroid, 433 Eros. The Multi-Spectral Imager (MSI) on the Near-Earth Asteroid Rendezvous (NEAR) spacecraft uses a five-element refractive optical telescope, has a field of view of 2.93 × 2.25°, a focal length of 167.35 mm, and has a spatial resolution of 16.1 × 9.5 m at a range of 100 km. The spectral sensitivity of the instrument spans visible to near infrared wavelengths, and was designed to provide insight into the nature and fundamental properties of asteroids and comets. Seven narrow band spectral filters were chosen to provide multicolor imaging and to make comparative studies with previous observations of S asteroids and measurements of the characteristic absorption in Fe minerals near 1 µm. An eighth filter with a much wider spectral passband will be used for optical navigation and for imaging faint objects, down to visual magnitude of +10.5. The camera has a fixed 1 Hz frame rate and the signal intensities are digitized to 12 bits. The detector, a Thomson-CSF TH7866A Charge-Coupled Device, permits electronic shuttering which effectively varies the dynamic range over an additional three orders of magnitude. Communication with the NEAR spacecraft occurs via a MIL-STD-1553 bus interface, and a high speed serial interface permits rapid transmission of images to the spacecraft solid state recorder. Onboard image processing consists of a multi-tiered data compression scheme. The instrument was extensively tested and calibrated prior to launch; some inflight calibrations have already been completed. This paper presents a detailed overview of the Multi-Spectral Imager and its objectives, design, construction, testing and calibration. 相似文献
997.
Markus J. Aschwanden Norma B. Crosby Michaila Dimitropoulou Manolis K. Georgoulis Stefan Hergarten James McAteer Alexander V. Milovanov Shin Mineshige Laura Morales Naoto Nishizuka Gunnar Pruessner Raul Sanchez A. Surja Sharma Antoine Strugarek Vadim Uritsky 《Space Science Reviews》2016,198(1-4):47-166
998.
P. C. Frisch M. Bzowski E. Grün V. Izmodenov H. Krüger J. L. Linsky D. J. McComas E. Möbius S. Redfield N. Schwadron R. Shelton J. D. Slavin B. E. Wood 《Space Science Reviews》2009,146(1-4):235-273
Interstellar material (ISMa) is observed both inside and outside of the heliosphere. Relating these diverse sets of ISMa data provides a richer understanding of both the interstellar medium and the heliosphere. The galactic environment of the Sun is dominated by warm, low-density, partially ionized interstellar material consisting of atoms and dust grains. The properties of the heliosphere are dependent on the pressure, composition, radiation field, ionization, and magnetic field of ambient ISMa. The very low-density interior of the Local Bubble, combined with an expanding superbubble shell associated with star formation in the Scorpius-Centaurus Association, dominate the properties of the local interstellar medium (LISM). Once the heliosphere boundaries and interaction mechanisms are understood, interstellar gas, dust, pickup ions, and anomalous cosmic rays inside of the heliosphere can be directly compared to ISMa outside of the heliosphere. Our understanding of ISMa at the Sun is further enriched when the circumheliospheric interstellar material is compared to observations of other nearby ISMa and the overall context of our galactic environment. The IBEX mission will map the interaction region between the heliosphere and ISMa, and improve the accuracy of comparisons between ISMa inside and outside the heliosphere. 相似文献
999.
D. Winterhalter M. Neugebauer B. E. Goldstein E. J. Smith B. T. Tsurutani S. J. Bame A. Balogh 《Space Science Reviews》1995,72(1-2):201-204
Data obtained by the Ulysses magnetometer and solar wind analyzer have been combined to study the properties of magnetic holes in the solar wind between 1 and 5.4 AU and to 23° south latitude. Although the plasma surrounding the holes was generally stable against the mirror instability, there are indications that the holes may have been remnants of mirror mode structures created upstream of the points of observation. Those indications include: (1) For the few holes for which proton or alpha-particle pressure could be measured inside the hole, the ion thermal pressure was always greater than in the plasma adjacent to the holes. (2) The plasma surrounding many of the holes was marginally stable for the mirror mode, while the plasma environment of all the holes was significantly closer to mirror instability than was the average solar wind. (3) The plasma containing trains of closely spaced holes was closer to mirror instability than was the plasma containing isolated holes. (4) The near-hole plasma had much higher ion (ratio of thermal to magnetic pressure) than did the average solar wind. 相似文献
1000.
H. U. Auster K. H. Glassmeier W. Magnes O. Aydogar W. Baumjohann D. Constantinescu D. Fischer K. H. Fornacon E. Georgescu P. Harvey O. Hillenmaier R. Kroth M. Ludlam Y. Narita R. Nakamura K. Okrafka F. Plaschke I. Richter H. Schwarzl B. Stoll A. Valavanoglou M. Wiedemann 《Space Science Reviews》2008,141(1-4):235-264