全文获取类型
收费全文 | 4203篇 |
免费 | 673篇 |
国内免费 | 986篇 |
专业分类
航空 | 2686篇 |
航天技术 | 1070篇 |
综合类 | 722篇 |
航天 | 1384篇 |
出版年
2024年 | 11篇 |
2023年 | 18篇 |
2022年 | 98篇 |
2021年 | 123篇 |
2020年 | 115篇 |
2019年 | 78篇 |
2018年 | 94篇 |
2017年 | 108篇 |
2016年 | 100篇 |
2015年 | 162篇 |
2014年 | 227篇 |
2013年 | 287篇 |
2012年 | 321篇 |
2011年 | 334篇 |
2010年 | 281篇 |
2009年 | 303篇 |
2008年 | 274篇 |
2007年 | 211篇 |
2006年 | 203篇 |
2005年 | 174篇 |
2004年 | 187篇 |
2003年 | 199篇 |
2002年 | 238篇 |
2001年 | 257篇 |
2000年 | 208篇 |
1999年 | 138篇 |
1998年 | 175篇 |
1997年 | 119篇 |
1996年 | 118篇 |
1995年 | 91篇 |
1994年 | 101篇 |
1993年 | 99篇 |
1992年 | 75篇 |
1991年 | 90篇 |
1990年 | 66篇 |
1989年 | 78篇 |
1988年 | 38篇 |
1987年 | 21篇 |
1986年 | 14篇 |
1985年 | 10篇 |
1984年 | 4篇 |
1983年 | 2篇 |
1982年 | 6篇 |
1981年 | 3篇 |
1980年 | 1篇 |
1965年 | 2篇 |
排序方式: 共有5862条查询结果,搜索用时 46 毫秒
941.
942.
针对航母机载武器弹药调度存在的过程复杂、不确定性强、涉及因素多等特点,建立了现阶段机载武器弹药调度模型。通过设计编码方案,选择适应度函数,设定交叉、变异操作建立了基于遗传算法的调度优化模型,并通过 Matlab软件进行了仿真验证。结果表明,该优化过程可在一定程度上缩短调度总时间,提高调度效率。 相似文献
943.
以长三角地区作为研究区域,提出了使用深度学习算法来实现主被动遥感数据结合反演地表PM2.5浓度的方法。基于MPL观测数据,使用雾霾层高度(HLH)替换了边界层高度(BLH)特征,对已有的基于气溶胶光学厚度(AOD)结合大气BLH来反演PM2.5浓度的算法进行了改进。为提高数据覆盖率,对研究区域内的MAIAC AOD进行了填补与评估。利用多种机器学习算法实现了日间逐小时的PM2.5浓度估算,模型验证相关性最高可达0.87。该方法能够为观测气候变化、应对大气污染提供有效帮助。 相似文献
944.
945.
开展高紫外-可见-近红外反射能力热控填料的制备,研制新型低吸收比(α_S)高发射率(ε_H)无机热控涂层。以自制SBA-15和ZnO前驱体为原料通过溶剂热浸渍和高温煅烧法制备ZnO/SBA-15填料,然后与硅酸钾(K_2SiO_3)制备无机热控涂层;采用SAXD、XRD、SEM、太阳反射光谱分析填料和涂层的性能。结果显示采用硝酸锌作为前驱体、m(ZnO)∶m(SBA-15)=3∶7、950℃下烧结3 h可以得到高紫外-可见-近红外反射能力的填料;ZnO/SBA-15/K_2SiO_3无机涂层的α_S为0.09,ε_H为0.91,涂层结合力等级为1级,经过100次-196~100℃热循环实验后,涂层无脱落和开裂现象。SBA-15改性ZnO可以获得具有高紫外反射率和低α_S的热控填料,ZnO/SBA-15填料制备的无机热控涂层同样具备高紫外反射率、低α_S和高ε_H,可以满足航天器高效散热的需求,应用前景良好。 相似文献
946.
This paper studies the proximate satellite interception guidance strategies where both the interceptor and target can perform orbital maneuvers with magnitude limited thrusts. This problem is regarded as a pursuit-evasion game since satellites in both sides will try their best to capture or escape. In this game, the distance of these two players is small enough so that the highly nonlinear earth-centered gravitational dynamics can be reduced to the linear Clohessy-Wiltshire (CW) equations. The system is then simplified by introducing the zero effort miss variables. Saddle solution is formulated for the pursuit-evasion game and time-to-go is estimated similarly as that for the exo-atmospheric interception. Then a vector guidance is derived to ensure that the interception can be achieved in the optimal time. The proposed guidance law is validated by numerical simulations. 相似文献
947.
948.
基于状态的维修着眼于系统的具体运行状况,对被监测装备的真实状态进行评估,克服了维修的盲目性,可有效减少由于维修不足而引起的意外故障和由于维修过剩带来的资源浪费。提出一种基于状态的多部件系统非周期预防性维修计划的优化方法,引入"机会维修阈值"概念,优化不同维修方式转移概率的表达式,将多个维修作业按照机会维修阈值进行归并,运用马尔可夫决策过程理论,给出不同维修方式转移概率的表达式和目标函数,并进行算例分析。结果表明:提出的优化模型减少了预防性维修活动,节约了维修工时和经费,可为系统预防性维修策略决策提供参考。 相似文献
949.
LIU Siqing ZHONG Qiuzhen GONG Jiancun SHI Liqin CHEN Dong MIAO Juan CAI Yanxia BAI Meng MA Wenzhen LI Zhitao LIU Fanghua CHEN Yanhong 《空间科学学报》2018,38(5):781-787
Strategic Priority Research Program on Space Science has gained remarkable achievements. Space Environment Prediction Center (SEPC) affiliated with the National Space Science Center (NSSC) has been providing space weather services and helps secure space missions. Presently, SEPC is capable to offer a variety of space weather services covering many phases of space science missions including planning, design, launch, and orbital operation. The service packages consist of space weather forecasts, warnings, and effect analysis that can be utilized to avoid potential space weather hazard or reduce the damage caused by space storms, space radiation exposure for example. Extensive solar storms that occurred over Chinese Ghost Festival (CGF) in September 2017 led to a large enhancement of the solar energetic particle flux at 1 AU, which affected the near Earth radiation environment and brought great threat to orbiting satellites. Based on the space weather service by SEPC, satellite ground support groups collaborating with the space Tracking, Telemetering and Command system (TT&C) team were able to take immediate measures to react to the CGF solar storm event. 相似文献
950.
Modeling and experimental validation of sawing based lander anchoring and sampling methods for asteroid exploration 总被引:1,自引:0,他引:1
Jun Zhang Chengcheng Dong Hui Zhang Song Li Aiguo Song 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(9):2426-2443
This paper presents a novel lander anchoring system based on sawing method for asteroid exploration. The system is composed of three robotic arms, three cutting discs, and a control system. The discs mounted at the end of the arms are able to penetrate into the rock surface of asteroids. After the discs cut into the rock surface, the self-locking function of the arms provides forces to fix the lander on the surface. Modeling, trajectory planning, simulations, mechanism design, and prototype fabrication of the anchoring system are discussed, respectively. The performances of the system are tested on different kinds of rocks, at different sawing angles, locations, and speeds. Results show that the system can cut 15?mm deep into granite rock in 180?s at sawing angle of 60°, with the average power of 58.41?W, and the “weight on bit” (WOB) of 8.637?N. The 7.8?kg anchoring system is capable of providing omni-directional anchoring forces, at least 225?N normal and 157?N tangent to the surface of the rock. The system has the advantages of low-weight, low energy consumption and balance forces, high anchoring efficiency and reliability, and could enable the lander to move and sample or assist astronauts and robots in walking and sampling on asteroids. 相似文献