全文获取类型
收费全文 | 523篇 |
免费 | 153篇 |
国内免费 | 44篇 |
出版年
2024年 | 4篇 |
2023年 | 1篇 |
2022年 | 5篇 |
2021年 | 18篇 |
2020年 | 8篇 |
2019年 | 10篇 |
2018年 | 6篇 |
2017年 | 21篇 |
2016年 | 25篇 |
2015年 | 12篇 |
2014年 | 29篇 |
2013年 | 52篇 |
2012年 | 23篇 |
2011年 | 34篇 |
2010年 | 22篇 |
2009年 | 35篇 |
2008年 | 35篇 |
2007年 | 34篇 |
2006年 | 39篇 |
2005年 | 45篇 |
2004年 | 30篇 |
2003年 | 34篇 |
2002年 | 27篇 |
2001年 | 18篇 |
2000年 | 17篇 |
1999年 | 21篇 |
1998年 | 24篇 |
1997年 | 11篇 |
1996年 | 12篇 |
1995年 | 14篇 |
1994年 | 9篇 |
1993年 | 10篇 |
1992年 | 6篇 |
1991年 | 5篇 |
1990年 | 21篇 |
1989年 | 3篇 |
排序方式: 共有720条查询结果,搜索用时 0 毫秒
201.
202.
行车取力泵控马达发电系统可以改变现有装备车辆供电模式。针对泵控马达系统存在转速和外接负载扰动的问题,以输入变转速变负载变量泵-定量马达恒速控制系统为研究平台,建立系统的流量模型,确定了对转速和负载扰动的控制策略以及相应的前馈补偿系数,采用了PID闭环控制与前馈补偿相结合的复合控制方法。并通过Matlab的Simulink模块对建立系统的仿真模型,得到了系统在转速和负载扰动下的控制规律,结果表明控制系统在两种扰动下反应迅速,最后通过实验验证,马达输出转速能保持在较理想的状态,为行车取力发电系统实现提供了借鉴意义。 相似文献
203.
应用冯.卡门功率谱和谐波合成法生成了考虑脉动效应的瞬时风速时程曲线;计算了发射筒各段的等效风压及等效力矩,给出了作用于发射筒迎风面的风压总值及等效力矩;最后将载荷作为输入条件,进行动力学分析,获得了风载荷作用下发射装置的动态响应。通过分析可知:由于发射装置具有刚度强、质量大的特点,风载荷作用下发射装置的速度、加速度响应均较低,因此,风载荷主要影响发射筒的倾斜程度。 相似文献
204.
Statistical analysis for masked system life data from Marshall‐Olkin Weibull distribution under progressive hybrid censoring
下载免费PDF全文
![点击此处可从《海军后勤学研究》网站下载免费的PDF全文](/ch/ext_images/free.gif)
This paper considers the statistical analysis of masked data in a series system, where the components are assumed to have Marshall‐Olkin Weibull distribution. Based on type‐I progressive hybrid censored and masked data, we derive the maximum likelihood estimates, approximate confidence intervals, and bootstrap confidence intervals of unknown parameters. As the maximum likelihood estimate does not exist for small sample size, Gibbs sampling is used to obtain the Bayesian estimates and Monte Carlo method is employed to construct the credible intervals based on Jefferys prior with partial information. Numerical simulations are performed to compare the performances of the proposed methods and one data set is analyzed. 相似文献
205.
针对伞翼无人机参数不确定性和复杂环境干扰敏感的问题,提出一种伞翼无人机线性自抗扰(Linear Active Disturbance Rejection Control,LADRC)高度控制方法。建立伞翼无人机8自由度飞行动力学模型,并引入风场和降雨模型以更加准确地模拟真实飞行环境。基于LADRC确定总体控制架构,设计线性扩张状态观测器对所有扰动进行估计,并引入误差反馈率在控制中实时补偿。使用该控制方法在多种扰动工况下进行伞翼无人机高度控制仿真实验。仿真结果表明,基于LADRC的高度控制方法能够有效克服内扰和外扰的影响,实现高精度高度控制;与传统PID控制效果相比,LADRC控制器具有更好的抗扰能力和鲁棒性。 相似文献
206.
《防务技术》2022,18(11):2034-2044
As an essential component of ammunition, pyrotechnics can control ignition with high reliability. However, due to limits of fabrication technology, traditional pyrotechnics are bulky. To achieve both functionality and miniaturization, MEMS pyrotechnics integrate initiator, safety-and-arming (S&A) device and lead charge and keep all components within a small size. MEMS S&A devices, as the core component to ensure system safety, are difficult to achieve active and rapid response to control signals with high safety and reliability. In order to overcome the difficulty, we propose the design and characterization of a MEMS pyrotechnic with a double-layer barrier S&A device. The MEMS pyrotechnic is a high-integrated device with an overall size of 13.4 × 8.5 × 5.2 mm3. The initiator is a NiCr bridge foil covered with an Al/CuO energetic film, which can generate flame when ignited by an excitation voltage. To match the flame energy, lead styphnate is chosen in this study as the lead charge. The S&A device contains four semi-circular barriers, which are directly driven by V-shape electro-thermal actuators to gain active control of the pyrotechnics' ignition condition with rapid response. To improve the system's reliability, the four barriers are axisymmetrically placed in two layers, two barriers for each layer, to constitute a double-layer structure with a thickness of 100 μm. The ignition test results show that the S&A device can prevent the initiator from detonating the lead charge in safety condition. In arming condition, the lead charge will be detonated. 相似文献
207.
《防务技术》2014,10(1):34-39
For the chip integration of MEMS (micro-electromechanical system) safety and arming device, a miniature detonator needs to be developed to reduce the weight and volume of explosive train. A Si-based micro-detonator is designed and fabricated, which meets the requirement of MEMS safety and arming device. The firing sensitivity of micro-detonator is tested according to GJB/z377A-94 sensitivity test methods: Langlie. The function time of micro-detonator is measured using wire probe and photoelectric transducer. The result shows the average firing voltage is 6.4 V when the discharge capacitance of firing electro-circuit is 33 μF. And the average function time is 5.48 μs. The firing energy actually utilized by Si-based micro-detonator is explored. 相似文献
208.
209.
210.