全文获取类型
收费全文 | 459篇 |
免费 | 96篇 |
国内免费 | 83篇 |
专业分类
航空 | 338篇 |
航天技术 | 115篇 |
综合类 | 26篇 |
航天 | 159篇 |
出版年
2024年 | 1篇 |
2023年 | 7篇 |
2022年 | 30篇 |
2021年 | 30篇 |
2020年 | 14篇 |
2019年 | 21篇 |
2018年 | 21篇 |
2017年 | 30篇 |
2016年 | 16篇 |
2015年 | 26篇 |
2014年 | 21篇 |
2013年 | 23篇 |
2012年 | 25篇 |
2011年 | 22篇 |
2010年 | 39篇 |
2009年 | 38篇 |
2008年 | 29篇 |
2007年 | 20篇 |
2006年 | 26篇 |
2005年 | 19篇 |
2004年 | 21篇 |
2003年 | 18篇 |
2002年 | 13篇 |
2001年 | 8篇 |
2000年 | 11篇 |
1999年 | 15篇 |
1998年 | 22篇 |
1997年 | 11篇 |
1996年 | 8篇 |
1995年 | 3篇 |
1994年 | 3篇 |
1993年 | 7篇 |
1992年 | 4篇 |
1991年 | 6篇 |
1990年 | 6篇 |
1989年 | 3篇 |
1988年 | 4篇 |
1987年 | 2篇 |
1985年 | 1篇 |
1984年 | 2篇 |
1983年 | 4篇 |
1982年 | 1篇 |
1981年 | 2篇 |
1979年 | 1篇 |
1971年 | 1篇 |
1970年 | 1篇 |
1969年 | 1篇 |
1968年 | 1篇 |
排序方式: 共有638条查询结果,搜索用时 46 毫秒
41.
E. Costa M. Salvati G. Agnetta R. Di Raffaele G. Gerardi B. Sacco L. Scarsi E. Massaro B. Agrinier J.C. Christi J.L. Masnou A. Bui-Van J.P. Chabaud P. Frabel P. Mandrou J. Narbonne M. Niel G. Rouaix G. Vedrenne 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1983,3(4):113-116
We present a large area, balloon borne, NaI(Tl) detector for low-energy gamma rays with temporal signature : FIGARO.The main detector is a mosaic of 12 NaI(Tl) tiles 22.5 × 15 × 5 cm, for a total geometric area of 4050 cm2.In the energy band 140 keV - 6 MeV, the expected background counting rate at float altitude is in the range of two to three thousands counts per second.For pulsar analysis the expected 3δ sensitivity for 5 hours exposition time is 2.5 10?4 ph/cm2.s.MeV (150–500 keV) 1.5 10?4 ph/cm2.s.MeV (1–6 MeV). This performance, together with the large effective area and the relatively short duration of a balloon flight, make FIGARO particularly suitable for the identification of sources by means of temporal analysis.For objectives in the Northern sky, including the Crab pulsar, a transmediterranean flight is planned for the summer of 1982 ; a Southern mission is scheduled in Brazil for the fall of 1983 (Vela, PSR 1822-09). 相似文献
42.
The difficult problem of synthesizing an optimal regulation scheme for linear time-invariant systems, assuming an integral quadratic cost functional, when the desired output is a constant nonzero vector and when the upper time limit approaches infinity, is studied in this paper. The problem is solved by properly redefining the cost functional, so that consistence with the stability requirement is achieved. The problem of the optimal closed-loop regulation of a singleinput/single-output system has always been an interesting topic for control engineers. The most common assumption is that the cost functional to minimize be of quadratic type, with infinity as an upper limit. The classical frequency domain approach, assuming the absence of initial conditions, suggests an optimal compensator in forward loop. On the other hand, the modern time-domain approach, based on the direct application of the maximum principle, yields a closed-form solution for the case in which the desired output is zero. This paper presents results which allow one to consider from a unifying point of view the two above approaches and, in addition, suggests a stable optimal scheme which is valid for any initial state and for any desired constant output. 相似文献
43.
A new thermo mechanical model for fiber fabric of hypervelocity impact is established by using the Johnson Cook model, the Gruneisen equation of state and the FEM SPH coupling algorithm, while some new factors are taken into account such as the heat generation, strain rate strengthening and high temperature softening of materials. Mechanical and thermal information could be obtained with the model, such as penetration, fragmentation, stress and strain, heat generation and temperature field of fiber fabric. The analysis results are in good agreement with the experimental results. 相似文献
44.
45.
F. Di Capua L. Campajola P. Casolaro M. Campajola A. Aloisio A. Lucaroni G. Furano A. Menicucci S. Di Mascio F. Malatesta M. Ottavi 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2019,63(10):3249-3257
A new methodology for Total Ionizing Dose (TID) tests is proposed. It is based on the employment of an on-chip 90Sr/90Y beta source as alternative to standard methods such as 60Co gamma rays and electrons from LINAC. The use of a compact beta source for TID tests has several advantages. In particular, the irradiation of devices with more than one radiation source results in a better representation of the complex space radiation environment composed of several types, energies and dose-rates. In addition, the use of an easy handling beta source allows the irradiation of electronic devices without any damage to other auxiliary circuit. In this work, 90Sr/90Y beta source dosimetry and related radiation field characteristics are discussed in depth.In order to validate the proposed source for TID tests, a rather complex device such as the “SPC56EL70L5” microcontroller from ST-Microelectronics was exposed to 90Sr/90Y beta rays. The results of this test were compared to that of a previous test of another sample from the same lot with a standard gamma 60Co source. The electronic performances following the two irradiations have been found to be in excellent agreement, by demonstrating therefore the validity of the proposed beta source for TID tests. 相似文献
46.
改善反作用轮低速性能的补偿观测器方法 总被引:3,自引:0,他引:3
基于Dahl摩擦模型,给出了用于卫星姿态三轴稳定控制的反作用轮低速动力学方程,就反作用轮转速过零对卫星姿态产生的扰动现象进行了分析,提出了一种利用非线性观测器估计摩擦力矩,并予以补偿的补偿观测器方法。仿真结果表明,该方法改善了反作用轮低速性能,提高了卫星姿态控制的指向精度和稳定度。 相似文献
47.
48.
就带有混合高斯测量噪声的离散时间系统 ,提出了一种简化的多模型滤波。理论分析证明该滤波方法用较少的计算量得到了与交互多模型滤波相同的估计性能。为满足应用要求 ,给出了该滤波器的数值鲁棒实现方法。一个关于仅有方位测量的制导例子验证了该滤波算法的有效性。 相似文献
49.
针对月球科研站任务地月遥操作需求和特点,设计地月准实时遥操作模拟验证系统,对其中的关键技术海量多尺度遥感数据环境感知、空地协同高精度定位、基于混合现实的预测仿真等进行了研究。提出了基于海量多尺度遥感数据的联合处理方法,环境感知数据融合可处理米级至厘米级环境感知结果;设计基于空地多运动平台协同定位的原型软件,空地协同地标约束下,定位精度不低于轨道器影像1个像素;开发了带有力觉反馈的预测仿真验证平台,在2~3 s变时延约束下可在仿真环境下协同演示遥操作过程,真实还原从端的遥操作作业场景,提高遥操作的执行效率和安全性。为地面人员的方案设计、操作手训练、故障处置等提供实时支持,为我国未来实施月球科研站任务筑牢基础。 相似文献
50.
针对拦截临近空间高速机动目标,基于有限时间理论,设计了有限时间收敛末制导律和脉冲宽度脉冲频率(PWPF)调节器。首先,介绍了加入PWPF调节器的末制导数学模型及工作原理;其次,设计了有限时间收敛制导律,应用有限时间理论证明了收敛条件和性质,并推广到推力受限条件下;最后,考虑视线(LOS)角速率快速收敛和发动机最小工作时间要求,设计了PWPF调节器参数。仿真结果表明,视线角速率在制导结束前的有限时间收敛至零,对目标机动具有鲁棒性,具有较高的制导精度,避免了发动机频繁开启,节省了燃料。 相似文献