全文获取类型
收费全文 | 631篇 |
免费 | 133篇 |
国内免费 | 246篇 |
专业分类
航空 | 600篇 |
航天技术 | 167篇 |
综合类 | 85篇 |
航天 | 158篇 |
出版年
2024年 | 5篇 |
2023年 | 28篇 |
2022年 | 45篇 |
2021年 | 46篇 |
2020年 | 61篇 |
2019年 | 42篇 |
2018年 | 33篇 |
2017年 | 33篇 |
2016年 | 44篇 |
2015年 | 52篇 |
2014年 | 65篇 |
2013年 | 56篇 |
2012年 | 49篇 |
2011年 | 68篇 |
2010年 | 53篇 |
2009年 | 63篇 |
2008年 | 40篇 |
2007年 | 38篇 |
2006年 | 33篇 |
2005年 | 34篇 |
2004年 | 25篇 |
2003年 | 17篇 |
2002年 | 16篇 |
2001年 | 17篇 |
2000年 | 6篇 |
1999年 | 5篇 |
1998年 | 6篇 |
1997年 | 2篇 |
1996年 | 5篇 |
1995年 | 6篇 |
1994年 | 5篇 |
1993年 | 1篇 |
1991年 | 1篇 |
1990年 | 1篇 |
1989年 | 3篇 |
1988年 | 3篇 |
1986年 | 1篇 |
1985年 | 2篇 |
排序方式: 共有1010条查询结果,搜索用时 15 毫秒
421.
422.
423.
可重复使用运载器(RLV)是未来实现快速、可靠及廉价进出空间的必然趋势,也是当前航空航天领域的研究热点。对RLV再入段的轨迹优化、制导及控制方法进行了综述。在RLV再入轨迹优化方法上,分别从间接法、直接法以及伪谱法等方面进行了综述,在深入分析每类方法特点的基础上,对其未来发展趋势进行了展望;在RLV再入制导方法上,分别从离线标称轨迹制导、在线轨迹重构制导、预测校正制导等方面进行了综述,对每类再入制导方法进行了优缺点分析,并对未来发展方向进行了总结;在RLV再入姿态控制方法上,分别从线性控制方法、非线性控制方法、智能控制方法等方面对其进行了综述,并对其特点和未来发展趋势进行了分析。最后,对RLV再入制导控制一体化方法进行了综述,指出了未来RLV制导控制一体化研究中亟需解决的关键问题。 相似文献
424.
425.
航空运输业排放环境影响评估研究 总被引:1,自引:0,他引:1
陈林 《中国民航学院学报》2011,(6):38-41
利用ICAO发动机排放数据库构建了航空运输业排放环境外部成本测算模型,并选取首都国际机场等6个国际机场作为实证研究的对象,测算了其2008年排放产生的环境外部成本,可以看出中国机场普遍存在着显著的排放环境外部成本。同时,针对中国航空运输业的发展现状,提出了通过实施排放权交易制度将中国航空运输业环境外部成本内部化的政策建议。研究成果可用于中国航空运输业排放环境外部成本的测算和治理。 相似文献
426.
427.
Three-dimensional path planning for unmanned aerial vehicle based on interfered fluid dynamical system 总被引:1,自引:0,他引:1
This paper proposes a method for planning the three-dimensional path for low-flying unmanned aerial vehicle(UAV) in complex terrain based on interfered fluid dynamical system(IFDS) and the theory of obstacle avoidance by the flowing stream. With no requirement of solutions to fluid equations under complex boundary conditions, the proposed method is suitable for situations with complex terrain and different shapes of obstacles. Firstly, by transforming the mountains, radar and anti-aircraft fire in complex terrain into cylindrical, conical, spherical, parallelepiped obstacles and their combinations, the 3D low-flying path planning problem is turned into solving streamlines for obstacle avoidance by fluid flow. Secondly, on the basis of a unified mathematical expression of typical obstacle shapes including sphere, cylinder, cone and parallelepiped, the modulation matrix for interfered fluid dynamical system is constructed and 3D streamlines around a single obstacle are obtained. Solutions to streamlines with multiple obstacles are then derived using weighted average of the velocity field. Thirdly, extra control force method and virtual obstacle method are proposed to deal with the stagnation point and the case of obstacles’ overlapping respectively. Finally, taking path length and flight height as sub-goals, genetic algorithm(GA) is used to obtain optimal 3D path under the maneuverability constraints of the UAV. Simulation results show that the environmental modeling is simple and the path is smooth and suitable for UAV. Theoretical proof is also presented to show that the proposed method has no effect on the characteristics of fluid avoiding obstacles. 相似文献
428.
429.
430.
Hypersonic glide vehicles (HGVs) are launched by a solid booster and glide through the atmosphere at high speeds. HGVs will be important means for rapid long-range delivery in the future. Given that the glide is unpowered, the initial glide conditions (IGCs) are crucial for flight. This paper aims to find the optimal IGCs to improve the maneuverability and decrease the con- straints of HGVs. By considering the IGCs as experiment factors, we design an orthogonal table with three factors that have five levels each by using the orthogonal experimental design method. Thereafter, we apply the Gauss pseudospectral method to perform glide trajectory optimization by using each test of the orthogonal table as the initial condition. Based on the analytic hierarchy process, an integrated indicator is established to evaluate the IGCs, which synthesizes the indexes of the maneuverability and constraints. The integrated indicator is calculated from the trajectory opti- mization results. Finally, optimal IGCs and valuable conclusions are obtained by using range anal- ysis, variance analysis, and regression analysis on the integrated indicator. 相似文献