全文获取类型
收费全文 | 7184篇 |
免费 | 14篇 |
国内免费 | 16篇 |
专业分类
航空 | 3333篇 |
航天技术 | 2579篇 |
综合类 | 23篇 |
航天 | 1279篇 |
出版年
2021年 | 57篇 |
2018年 | 133篇 |
2017年 | 98篇 |
2016年 | 96篇 |
2015年 | 50篇 |
2014年 | 172篇 |
2013年 | 199篇 |
2012年 | 198篇 |
2011年 | 287篇 |
2010年 | 197篇 |
2009年 | 315篇 |
2008年 | 403篇 |
2007年 | 201篇 |
2006年 | 167篇 |
2005年 | 219篇 |
2004年 | 198篇 |
2003年 | 240篇 |
2002年 | 141篇 |
2001年 | 241篇 |
2000年 | 114篇 |
1999年 | 159篇 |
1998年 | 191篇 |
1997年 | 139篇 |
1996年 | 148篇 |
1995年 | 209篇 |
1994年 | 215篇 |
1993年 | 115篇 |
1992年 | 148篇 |
1991年 | 78篇 |
1990年 | 72篇 |
1989年 | 138篇 |
1988年 | 66篇 |
1987年 | 65篇 |
1986年 | 72篇 |
1985年 | 192篇 |
1984年 | 179篇 |
1983年 | 149篇 |
1982年 | 148篇 |
1981年 | 239篇 |
1980年 | 68篇 |
1979年 | 63篇 |
1978年 | 63篇 |
1977年 | 52篇 |
1976年 | 54篇 |
1975年 | 53篇 |
1974年 | 50篇 |
1973年 | 49篇 |
1972年 | 59篇 |
1971年 | 40篇 |
1970年 | 40篇 |
排序方式: 共有7214条查询结果,搜索用时 93 毫秒
41.
42.
Moisseev S. Soshin K. Nakaoka M. 《IEEE transactions on aerospace and electronic systems》2005,41(1):174-180
A novel high-frequency transformer linked full-bridge type soft-switching phase-shift pulsewidth modulated (PWM) controlled dc-dc power converter is presented, which can be used as a power conditioner for small-scale photovoltaic and fuel cell power generation systems as well as isolated boost dc-dc power converter for automotive ac power supply. In these applications with low-voltage large-current sources, the full-bridge circuit is the most attractive topology due to the possibility of using low-voltage high-performance metal-oxide-semiconductor field-effect transistor (MOSFET) and achieving high efficiency of the dc-dc power converter. A tapped-inductor filter including the freewheeling diode is newly implemented in the output stage of the full-bridge phase-shift PWM dc-dc converter to achieve soft-switching operation for the wide load variation range. Moreover, in the proposed converter circuit, the circulating current is effectively minimized without using additional resonant circuit and auxiliary power switching devices. The practical effectiveness of the proposed soft-switching dc-dc power converter was verified in laboratory level experiment with 1 kW 100 kHz breadboard setup using power MOSFETs. Actual efficiency of 94-97% was obtained for the wide duty cycle and load variation ranges. 相似文献
43.
44.
G. Paschmann M. Boehm H. Höfner R. Frenzel P. Parigger F. Melzner G. Haerendel C. A. Kletzing R. B. Torbert G. Sartori 《Space Science Reviews》1994,70(3-4):447-463
The Electron Beam Instrument (F6) onFreja is the first attempt to apply the electron drift technique in a region of large ambient magnetic fields. The paper describes the operational principles, the technical realization, and the difficulties encountered in the derivation of the electric fields. 相似文献
45.
The Cluster mission of the European Space Agency (ESA) will allow, for the first time three-dimensional measurements in key regions of the Earth's magnetosphere to be carried out. The European Numerical Simulation Network (ENSN) aims at providing a theoretical support to the mission. We describe the achievements of the ENSN during its first period of activity 1991–1994, during which the network was funded by the European Union. In particular, the ENSN has set up (i) thematic Working Groups on the prime scientific goals of the mission, (ii) a code development Working Group to develop numerical simulation codes specifically adapted to studying magnetospheric boundaries and the corresponding scale mixing, and (iii) software models of Cluster instruments to test in a numerical simulation what the set of four instruments will measure. 相似文献
46.
Eagle-Picher Energy Products (EPEP) has been manufacturing and testing large lithium ion cells (up to 100-Ah) for several years. Recently, work has focused on the testing of different chemistries at variable temperatures and designing and fabricating 100-Ah cylindrical cells. For the aircraft application the largest concern is irreversible capacity loss at elevated temperatures (70°C). In contrast, for the aerospace application shelf-life and cycle life are critical. EPEP has found that the major contributor to the loss in low temperature performance due to high temperature testing, was the positive electrode. EPEP discuss recent results of variable temperature cycling and 100-Ah cell performance 相似文献
47.
Senrad: an advanced wideband air-surveillance radar 总被引:1,自引:0,他引:1
Skolnik M. Linde G. Meads K. 《IEEE transactions on aerospace and electronic systems》2001,37(4):1163-1175
The generic characteristics and performance of an experimental long-range air-surveillance radar, known at the Naval Research Laboratory as Senrad, is described. Its distinguishing feature is that it can operate with simultaneous transmissions over a very wide bandwidth-from 850 to 1400 MHz. The technology and type of experimental radar equipment employed are discussed and examples are given of its performance capabilities obtained by means of very wideband operation. The unusually wide bandwidth of this radar allows 1) improved detection and tracking performance because of the absence of the nulls that are common in the antenna elevation radiation-pattern of a single-frequency radar; 2) moving target indication (MTI) without loss of targets due to blind speeds and without the need for multiple PRFs (pulse repetition frequencies); 3) accurate height finding with a fan-beam radar by taking advantage of the multipath time difference as a function of target height; 4) a form of limited target recognition based on high range-resolution; and 5) a reduction of the effectiveness of electronic countermeasures that can seriously degrade more narrowband radars 相似文献
48.
Bacon B.J. Ostroff A.J. Joshi S.M. 《IEEE transactions on aerospace and electronic systems》2001,37(4):1373-1383
A modified derivation of nonlinear dynamic inversion provides the theoretical underpinnings for a reconfigurable control law for aircraft that have suffered combinations of actuator failures, missing effector surfaces, and aerodynamic changes. The approach makes use of acceleration feedback to extract information pertaining to any aerodynamic change and thus does not require a complete aerodynamic model of the aircraft. The control law does require feedback of effector positions to accommodate actuator dynamics. Both accelerometer and rate gyro failure detection and isolation (FDI) systems are implemented, allowing up to three independent failures for each FDI system as long as they are in different axes. Nonlinear simulation results show that the FDI systems improve the robustness to accelerometer/rate gyro uncertainties. An advanced tailless aircraft model is used to demonstrate the concepts. The simulation includes accelerometer and rate gyro noise and bias, failures due to accelerometers, rate gyros, and actuators, and modeled missing surfaces that cause airplane aerodynamic changes 相似文献
49.
Shu-Mei Guo Shieh L.S. Guanrong Chen Coleman N.P. 《IEEE transactions on aerospace and electronic systems》2001,37(4):1406-1418
An observer-type of Kalman innovation filtering algorithm to find a practically implementable "best" Kalman filter, and such an algorithm based on the evolutionary programming (EP) optima-search technique, are proposed, for linear discrete-time systems with time-invariant unknown-but-hounded plant and noise uncertainties. The worst-case parameter set from the stochastic uncertain system represented by the interval form with respect to the implemented "best" filter is also found in this work for demonstrating the effectiveness of the proposed filtering scheme. The new EP-based algorithm utilizes the global optima-searching capability of EP to find the optimal Kalman filter and state estimates at every iteration, which include both the best possible worst case Interval and the optimal nominal trajectory of the Kalman filtering estimates of the system state vectors. Simulation results are included to show that the new algorithm yields more accurate estimates and is less conservative as compared with other related robust filtering schemes 相似文献
50.
The Freja ultraviolet imager 总被引:2,自引:0,他引:2
J. S. Murphree R A. King T. Payne K. Smith D. Reid J. Adema B. Gordon R. Wlochowicz 《Space Science Reviews》1994,70(3-4):421-446
Auroral images acquired by satellite instrumentation have proven to be a crucial component of the scientific equiry into the physical processes of the Earth's magnetosphere. TheFreja mission provided an opportunity to extend these measurements into the temporal and spatial regime commonly associated with ground-based optical imagers. Employing the basic procedure used successfully in theViking program allowed image repetition rates of 6 s to be achieved with simultaneous exposure of all pixels within the field-of-view. Typical exposure times of 0.3 s required development of an improved image intensifier system and operational requirements resulted in image formats covering approximately one-third of a spin. Simultaneously exposing two broad-band UV cameras, the instrument generates in its normal operational mode 264.6 kbytes per image pair. Results from initial operations confirm the design approach and suggest such imagers can be routinely included on challenging low cost missions such asFreja. 相似文献