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91.
验证码是一种标准的网络安全技术,它主要用来防止网民或者黑客等对网站的恶意注册和访问,以及发送垃圾文件、暴力破解高价值密码、滥发广告等恶意事件。通过对图片的扫描,可以提取图片中的数字、字符信息等。本文提出了一种基于OCR技术的图形验证码识别技术。通过对验证码图片进行灰度化、二值化、去噪点、圈点填充、直线填充、图像分割、统一大小、图像匹配和存入字库等一系列的操作,进行对验证码的识别实验。本文通过实验对验证码的特点有了充分的了解,这样方便设计出更加安全的验证码,防止被不法分子破解。 相似文献
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When an inter-area mode dominates a low-frequency oscillation in a stressed condition, control of the active power flow of interface lines, with compensating devices, can effectively reduce the electromechanical power oscillations. In general, interface lines in which inter-area oscillations are large are considered to be good locations for installation of compensating devices. A sensitivity analysis with respect to change in active power flow can provide an important factor in electric power system operation. This paper proposes a new methodology to calculate the damping sensitivity with respect to change in active power flow, which can be useful for accurate selection of critical lines from the viewpoint of small-signal stability. In the proposed methodology, a damping sensitivity index is used to select the critical lines to damp power system oscillations. This paper describes how to derive the damping sensitivity for the selected mode and illustrates an example applying the proposed algorithm to a simple two-area system and the New England 39-bus test system. 相似文献
94.
研究适合导弹自适应自动驾驶仪设计中对于参数快速变化的有效的辨识方法,从几种时变参数辨识方法的研究着手,经过适当的修改和组合,得出适用的辨识方法。通过从理论分析到微机仿真等一系列工作,证明了这一辨识方法能够较好跟踪导弹气动参数的变化。 相似文献
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基于标准水资源指数(SWRI)的流域水文干旱评估——以海河北系为例 总被引:2,自引:0,他引:2
构建了一个新的水文干旱评估指标——标准水资源指数(SWRI),结合分布式水循环模型、Copula函数及统计检验等方法,形成了一套完整的水文干旱识别、评估及特征分析的基本框架。以海河北系为例,定量识别了1956—2009年间的水文干旱事件,并对其干旱特征及变化规律进行了剖析。结果表明:海河北系近54年发生的34次水文干旱主要集中在短历时、低强度、小面积区间内,空间上主要分布在张家口、大同及北京等地区;干旱指标的联动关系上,干旱历时、强度与面积指标间呈显著的线性或指数相关关系,90%的水文干旱历时低于40个月、干旱面积占比不超过43%,干旱强度低于9.0;在给定的干旱特征指标值(如干旱面积)条件下,另一干旱指标值越大(如强度越大)干旱发生概率越小,且存在明显的特征区间;单变量水文干旱重现期介于联合重现期和同现重现期之间。 相似文献
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弹道式航天飞行器末修闭路制导飞行段通常采用具有非线性特性的固定姿控喷管进行姿态跟踪和稳定控制,此时姿态控制精度直接影响闭路制导效果。传统斜线开关线控制方法存在系统性姿态角偏差,导致末修推力方向与待增速度方向始终存在差异,进而影响到飞行器落点精度。提出的基于干扰力矩辨识的高精度非线性姿态控制方法,通过干扰力矩在线辨识,实时设计姿控喷管开关线,将极限环调整至环绕原点,从而提高姿控精度。基于某型飞行器的仿真结果表明,与传统设计方法相比,基于干扰力矩辨识的高精度非线性姿态控制方法可将闭路制导段姿态控制精度提高约90%,减小姿态偏差对闭路制导的影响,飞行器落点精度提高约25%。 相似文献
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《Journal of Process Control》2014,24(5):621-639
Complex, high performance, engineering systems have to be closely monitored and controlled to ensure safe operation and protect public from potential hazards. One of the main challenges in designing monitoring and control algorithms for these systems is that sensors and actuators may be malfunctioning due to malicious or natural causes. To address this challenge, this paper addresses a resilient monitoring and control (ReMAC) system by expanding previously developed resilient condition assessment monitoring systems and Kalman filter-based diagnostic methods and integrating them with a supervisory controller developed here. While the monitoring and diagnostic algorithms assess plant cyber and physical health conditions, the supervisory controller selects, from a set of candidates, the best controller based on the current plant health assessments. To experimentally demonstrate its enhanced performance, the developed ReMAC system is then used for monitoring and control of a chemical reactor with a water cooling system in a hardware-in-the-loop setting, where the reactor is computer simulated and the water cooling system is implemented by a machine condition monitoring testbed at Idaho National Laboratory. Results show that the ReMAC system is able to make correct plant health assessments despite sensor malfunctioning due to cyber attacks and make decisions that achieve best control actions despite possible actuator malfunctioning. Monitoring challenges caused by mismatches between assumed system component models and actual measurements are also identified for future work. 相似文献
100.
This paper considers the problem of controlling the position and the orientation of a Gun Launched Micro Aerial Vehicle – GLMAV – despite unknown aerodynamic efforts. The proposed approach overcomes the problem of gyroscopic coupling by taking advantage from the structure of the thrust mechanism, which is made up of two counter rotating propellers. An adaptive hierarchical controller is designed, allowing the trajectory tracking and the stabilization of the vehicle's position and orientation while the unknown aerodynamic efforts are estimated by means of an identifier. The overall process is shown to be stable for constant, or slowly time varying, aerodynamic efforts. However numerical simulations demonstrate the satisfying controller's performance even with nonconstant aerodynamic efforts. Experimental results are also provided. 相似文献