全文获取类型
收费全文 | 2127篇 |
免费 | 590篇 |
国内免费 | 308篇 |
专业分类
航空 | 1459篇 |
航天技术 | 629篇 |
综合类 | 288篇 |
航天 | 649篇 |
出版年
2024年 | 11篇 |
2023年 | 38篇 |
2022年 | 58篇 |
2021年 | 106篇 |
2020年 | 155篇 |
2019年 | 179篇 |
2018年 | 140篇 |
2017年 | 135篇 |
2016年 | 127篇 |
2015年 | 141篇 |
2014年 | 185篇 |
2013年 | 170篇 |
2012年 | 180篇 |
2011年 | 176篇 |
2010年 | 134篇 |
2009年 | 130篇 |
2008年 | 112篇 |
2007年 | 126篇 |
2006年 | 152篇 |
2005年 | 110篇 |
2004年 | 76篇 |
2003年 | 61篇 |
2002年 | 43篇 |
2001年 | 59篇 |
2000年 | 35篇 |
1999年 | 24篇 |
1998年 | 24篇 |
1997年 | 15篇 |
1996年 | 20篇 |
1995年 | 17篇 |
1994年 | 25篇 |
1993年 | 18篇 |
1992年 | 9篇 |
1991年 | 10篇 |
1990年 | 10篇 |
1989年 | 8篇 |
1988年 | 3篇 |
1987年 | 1篇 |
1986年 | 1篇 |
1984年 | 1篇 |
排序方式: 共有3025条查询结果,搜索用时 953 毫秒
681.
Sylvain Chaty 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
In this review I first describe the nature of the three kinds of High-Mass X-ray Binaries (HMXBs), accreting through: (i) Be circumstellar disc, (ii) supergiant stellar wind, and (iii) Roche lobe filling supergiants. 相似文献
682.
683.
自由飞行是解决空域拥挤问题的一种有效飞行模式。随着通信、导航、监视( CNS )技术的不断进步和自由飞行理论的不断完善,自由飞行将会使飞机由被动指挥向自选最优路径转变,能够明显提高空域的容量和飞行的效率。在评估自由飞行环境下飞机运行的安全性时,需要行之有效的碰撞风险评估方法。首先考虑通信、导航、监视(CNS)性能对飞机定位误差的影响,在执行飞行冲突解脱命令过程中引入相互作用粒子系统(IPS),提出一种自由飞行下飞机碰撞风险评估算法,最后结合目标安全水平寻找最优最小安全间距。算例表明,算法能够快速有效计算自由飞行下飞机间碰撞风险,具有可行性。 相似文献
684.
685.
686.
Zhang Zhengyang 《中国航空学报》1998,(3):214-219
A new remote sensing image coding scheme based on the wavelet transform and classified vector quantization (CVQ) is proposed. The original image is first decomposed into a hierarchy of 3 layers including 10 subimages by DWT. The lowest frequency subimage is compressed by scalar quantization and ADPCM. The high frequency subimages are compressed by CVQ to utilize the similarity among different resolutions while improving the edge quality and reducing computational complexity. The experimental results show that the proposed scheme has a better performance than JPEG, and a PSNR of reconstructed image is 31~33 dB with a rate of 0.2 bpp. 相似文献
687.
典型直升机是实施立体突击作战的重要力量,在火力支援、立体补给、综合勤务保障等方面发挥着重要作用。针对其构造形式和作战使用要求,直升机在低空超低空低速执行任务时,使用场景中面临低空和地面的多种威胁,致使其服役环境和作战环境更加恶劣。本文通过分析直升机在作战中面临的威胁特点,阐述在直升机设计和使用维护过程中,综合防护能力、环境适应能力、战伤抢修能力对直升机作战完整性的影响,通过合理设计机体结构,提升生存能力,提升海上、高原、沙尘等环境适应能力,建立完备的战伤抢修能力来保证直升机使用的完整性,满足使用需求。 相似文献
688.
G.P. Wu G.L. Huang Y. Huang D.Y. Wang 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(6):984-987
Based upon the most efficient electron acceleration near the midplane of 3D non-neutral driven reconnecting current sheet (RCS) and the electrostatic wave excitation by the drift Maxwellian distribution of electrons in Vlasov simulation, we assume that the electrostatic waves mainly propagate opposite to the reconnecting electric field and investigated how these waves affect the electron acceleration. The main results are: (1) when the electron’s velocity equals to the phase speed of the waves, they will be trapped and have the different accelerating characteristics from the untrapped electrons through solving the momentum equations of electrons analytically; (2) the test particle simulations further prove that the number of the energetic electrons decreases with the increasing intensity of unstable waves, and the distribution of the energetic electrons takes on the double power-law. 相似文献
689.
High-efficiency aircraft antiskid brake control algorithm via runway condition identification based on an on-off valve array 总被引:1,自引:1,他引:1
The aircraft antiskid braking system is an important hydraulic system for preventing tire bursts and ensuring safe take-off and landing. The brake system adjusts the force applied on the brake discs by controlling the brake pressure. Traditional aircraft antiskid braking systems achieve antiskid performance by controlling the braking pressure with an electrohydraulic servo valve. Because the pilot stage of an electrohydraulic servo valve is easily blocked by carbonized hydraulic oil, the servo valve would become a dangerous weak point for aircraft safety. This paper proposes a new approach that uses an on-off valve array to replace the servo valve for pressure control. Based on this new pressure control component, an efficient antiskid control algorithm that can utilize this discontinuous feature is proposed. Furthermore, the algorithm has the ability to identify the runway circumstances. To overcome the discontinuity in the process of using an on-off valve array, the Filippov framework is introduced. The conditions of convergence of the system are also discussed. The results of the digital simulations and the hardware-in-the-loop (HIL) braking experiments are used to verify the efficiency and stability of the proposed control algorithm. The method also proves that the on-off valve array can replace the servo valve perfectly as a new type of antiskid braking pressure control component. 相似文献
690.
Aerodynamic multi-objective integrated optimization based on principal component analysis 总被引:2,自引:0,他引:2
Based on improved multi-objective particle swarm optimization (MOPSO) algorithm with principal component analysis (PCA) methodology,an efficient high-dimension multiobjective optimization method is proposed,which,as the purpose of this paper,aims to improve the convergence of Pareto front in multi-objective optimization design.The mathematical efficiency,the physical reasonableness and the reliability in dealing with redundant objectives of PCA are verified by typical DTLZ5 test function and multi-objective correlation analysis of supercritical airfoil,and the proposed method is integrated into aircraft multi-disciplinary design (AMDEsign) platform,which contains aerodynamics,stealth and structure weight analysis and optimization module.Then the proposed method is used for the multi-point integrated aerodynamic optimization of a wide-body passenger aircraft,in which the redundant objectives identified by PCA are transformed to optimization constraints,and several design methods are compared.The design results illustrate that the strategy used in this paper is sufficient and multi-point design requirements of the passenger aircraft are reached.The visualization level of non-dominant Pareto set is improved by effectively reducing the dimension without losing the primary feature of the problem. 相似文献