全文获取类型
收费全文 | 2481篇 |
免费 | 2篇 |
国内免费 | 6篇 |
专业分类
航空 | 1220篇 |
航天技术 | 991篇 |
综合类 | 5篇 |
航天 | 273篇 |
出版年
2021年 | 13篇 |
2019年 | 14篇 |
2018年 | 40篇 |
2017年 | 34篇 |
2016年 | 25篇 |
2015年 | 11篇 |
2014年 | 50篇 |
2013年 | 60篇 |
2012年 | 50篇 |
2011年 | 87篇 |
2010年 | 62篇 |
2009年 | 105篇 |
2008年 | 149篇 |
2007年 | 62篇 |
2006年 | 46篇 |
2005年 | 62篇 |
2004年 | 71篇 |
2003年 | 91篇 |
2002年 | 46篇 |
2001年 | 101篇 |
2000年 | 45篇 |
1999年 | 86篇 |
1998年 | 85篇 |
1997年 | 62篇 |
1996年 | 63篇 |
1995年 | 88篇 |
1994年 | 97篇 |
1993年 | 37篇 |
1992年 | 59篇 |
1991年 | 22篇 |
1990年 | 28篇 |
1989年 | 56篇 |
1988年 | 20篇 |
1987年 | 35篇 |
1986年 | 19篇 |
1985年 | 74篇 |
1984年 | 42篇 |
1983年 | 46篇 |
1982年 | 55篇 |
1981年 | 77篇 |
1980年 | 26篇 |
1979年 | 24篇 |
1978年 | 22篇 |
1977年 | 18篇 |
1976年 | 15篇 |
1975年 | 18篇 |
1974年 | 12篇 |
1972年 | 17篇 |
1969年 | 13篇 |
1966年 | 8篇 |
排序方式: 共有2489条查询结果,搜索用时 265 毫秒
751.
Hernandez M. Ristic B. Farina A. Sathyan T. Kirubarajan T. 《IEEE transactions on aerospace and electronic systems》2008,44(2):724-747
This paper considers the theoretical posterior Cramer-Rao lower bound (PCRLB) for the case of tracking a manoeuvring target with Markovian switching dynamics. In a recent article [2] it was proposed to calculate the PCRLB conditional on the manoeuvre sequence and then determine the bound as a weighted average, giving an unconditional PCRLB. However, we demonstrate that this approach can produce an overly optimistic lower bound, because the sequence of manoeuvres is implicitly assumed known. Motivated by this, we develop a general approach and derive a closed-form estimate of the PCRLB in the case of Markovian switching systems. The basis of the approach is to, at each time step, replace the multi-modal prior target probability density function (pdf) with a best-fitting Gaussian (BFG) approximation. We present a recursive formula for calculating the mean and covariance of this Gaussian distribution, and demonstrate how the covariance increases as a result of the potential manoeuvres. We are then able to calculate the PCRLB for this BFG model using an existing Riccati-like recursion. Because of the BFG approximation, we are no longer guaranteed a bound and so we refer to our estimate as an "error performance measure" rather than a bound. The presented approach is applied both to filtering and smoothing cases. The simulation results indicate a very close agreement between the proposed performance measure and the error performance of an interacting multiple model estimator. 相似文献
752.
753.
R. Adachi T. Takaya K. Kuriyama A. Higashibata N. Ishioka H. Kagawa 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(5):816-823
We have investigated the effect of microgravity during spaceflight on body-wall muscle fiber size and muscle proteins in the paramyosin mutant of Caenorhabditis elegans. Both mutant and wild-type strains were subjected to 10 days of microgravity during spaceflight and compared to ground control groups. No significant change in muscle fiber size or quantity of the protein was observed in wild-type worms; where as atrophy of body-wall muscle and an increase in thick filament proteins were observed in the paramyosin mutant unc-15(e73) animals after spaceflight. We conclude that the mutant with abnormal muscle responded to microgravity by increasing the total amount of muscle protein in order to compensate for the loss of muscle function. 相似文献
754.
C. T. Bolton 《Space Science Reviews》1989,50(1-2):311-322
Variations in the magnetic pressure and flux blocking by starspots during the magnetic cycle of the cool semidetached component of an Algol binary may cause cyclic changes in the quadrupole moment and moment of inertia of the star which can cause alternate period changes. Since several different processes and timescales are involved, the orbital period changes may not correlate strongly with the indicators of magnetic activity. The structural changes in the semidetached component can also modulate the mass transfer rate. Sub-Keplerian velocities, supersonic turbulence, and high temperature regions in circumstellar material around the accreting star may all be a consequence of magnetic fields embedded in the flow. Models for the evolution of Algols which include the effects of angular momentum loss (AML) through a magnetized wind may have underestimated the AML rate by basing it on results from main sequence stars. Evolved stars appear to have higher AML rates, and there may be additional AML in a wind from the accretion disk. 相似文献
755.
The theory of a new type of vibratory rate gyroscope is considered. The design considered is based upon a disc of piezoelectric material on which are deposited drive and pick-off electrodes. The equations of motion of the disc are derived and the response of the gyroscope to constant and harmonic rates of turn determined. 相似文献
756.
T. G. Hawarden R. O. Cummings C. M. Telesco H. A. Thronson Jr 《Space Science Reviews》1992,61(1-2):113-144
General principles are outlined for the design of space infrared telescopes intended to cool by radiation to the lowest temperatures attainable without the use of on-board cryogens, and assuming on-orbit cooling after a warm launch. Maximum protection from solar and earth heating, maximum radiating area and efficiency and minimum absorbing area and absorptivity are the obvious basic criteria. The optimised design is a short, fat telescope surrounded by a series of radiation shields, each cooled by its own radiator. Maximising the longitudinal conductivity of the radiation shields and of the telescope tube itself is important both to the on-orbit cooling time and the final achieveable temperature. Realistic designs take between 80 and 200 days to cool to within a few degrees of equilibrium temperatures, depending on the materials used. Great advantages accrue from the use of an orbit distant from earth. Both simple models and detailed simulations suggest that temperatures of 30 to 40 K are attainable in high earth orbits. Placing a radiatively cooled telescope in a halo orbit around the Lagrangian point L2 is a particularly attractive option and significantly lower temperatures can be achieved there than in Earth orbit. Optimised radiative cooling is an important element of the small Japanese mission SMIRT. We suggest that a combination of an ESA Medium-sized Mission with a NASA Explorer to send a 2m+ telescope to an L2 halo orbit would provide a cost-effective and powerful long-duration facility for the early 21st century. 相似文献
757.
E. D. Feigelson S. Casanova T. Montmerle J. Guibert 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1993,13(12):311-314
Two soft X-ray images of the Chamaeleon I star forming cloud obtained with the ROSAT Position Sensitive Proportional Counter are presented. Seventy reliable, and perhaps 19 additional, X-ray sources are found. Up to Ninety percent of these sources are certainly or probably identified with T Tauri stars formed in the cloud. Twenty to 35 are probably previously unrecognized ‘weak’ T Tauri (WTT) stars. T Tauri X-ray luminosities range from log
, or 102 – 104 times solar levels, with mean
in the 0.2–2.5 keV band. The X-ray luminosities of well-studied Chamaeleon cloud members are correlated with a complex of four stellar properties: effective temperature, mass, radius and bolometric luminosity. The spatial distribution, H-R diagram locations of the stars indicate WTT and CTT are coeval. The total premain sequence population of the cloud is likely to be > 100 stars, with WTT stars outnumbering ‘classical’ T Tauri (CTT) stars by 2:1. 相似文献
758.
It is argued that the job of an automatic test equipment (ATE) technician is evolving toward that of a computer operator. The technician has automatic tools (test programs) written for every replaceable unit in his test set. The technician selects which test is run. During the test the technician is presented results and given options if a test fails. If the option called out by the test program does not fix the problem, the technician must go back into his tool box (his library of test programs) and select the right tool to do the job. This is true for a technician working on any piece of ATE. It is contended that training for these technicians should be centered around troubleshooting skills with initially less emphasis on the hardware implementation details. These skills could be developed with a genetic trainer 相似文献
759.
760.
A Johnsson T Eidesmo 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1989,9(11):273-281
Rhythmic phenomena in biology cover a wide frequency spectrum. In Space, the rhythms will encounter microgravity conditions which can, therefore, be a valuable tool for their understanding. A review and discussion of important effects of gravity/absence of gravity on biological systems will be given. Convection will be emphasized as a mechanism which is drastically reduced in Space. Microgravity might also affect the coupling between individual oscillators in a multi-oscillatory system. The environmental interference with rhythms will be discussed with a simple feedback as a starting point. Model simulations will be presented and clinostat and microgravity-conditions will be discussed in a specific case, viz. the gravitropical system of plants which can show sustained oscillations. 相似文献