全文获取类型
收费全文 | 672篇 |
免费 | 291篇 |
国内免费 | 69篇 |
专业分类
航空 | 576篇 |
航天技术 | 104篇 |
综合类 | 24篇 |
航天 | 328篇 |
出版年
2023年 | 17篇 |
2022年 | 35篇 |
2021年 | 32篇 |
2020年 | 39篇 |
2019年 | 17篇 |
2018年 | 22篇 |
2017年 | 15篇 |
2016年 | 24篇 |
2015年 | 21篇 |
2014年 | 43篇 |
2013年 | 54篇 |
2012年 | 44篇 |
2011年 | 47篇 |
2010年 | 37篇 |
2009年 | 15篇 |
2008年 | 25篇 |
2007年 | 46篇 |
2006年 | 36篇 |
2005年 | 48篇 |
2004年 | 35篇 |
2003年 | 26篇 |
2002年 | 23篇 |
2001年 | 24篇 |
2000年 | 27篇 |
1999年 | 41篇 |
1998年 | 31篇 |
1997年 | 33篇 |
1996年 | 30篇 |
1995年 | 39篇 |
1994年 | 19篇 |
1993年 | 16篇 |
1992年 | 14篇 |
1991年 | 19篇 |
1990年 | 10篇 |
1989年 | 17篇 |
1988年 | 4篇 |
1987年 | 7篇 |
排序方式: 共有1032条查询结果,搜索用时 15 毫秒
911.
912.
913.
李迈强 《西安航空技术高等专科学校学报》2007,25(1):9-13
为进一步推动陕西高职教育事业健康发展,在充分调查研究的基础上,对西安航专高职教育教学改革进行总结、分析,着重论述了西安航专教学改革的指手思想、主要目标、基本思路、主要做法及教学改革的主要成果。 相似文献
914.
新一代运载火箭控制系统总线 总被引:1,自引:0,他引:1
介绍了目前各种高速数据总线。主要包括火线、航天光纤数据总线、SpaceWire,光纤通道、FDDI,ATM,以太网等。对比了这些总线的特点和性能,并根据火箭控制系统的性能要求,对这些总线进行筛选。最终确定光纤通道作为新一代火箭控制系统总线的首选。 相似文献
915.
916.
This paper describes the end-to-end validation process for the Attitude Control Subsystem (ACS) of the satellite INTA-NanoSat-1B (NS-1B). This satellite was launched on July 2009 and it has been fully operative since then. The development of its ACS modules required an exhaustive integration and a system-level validation program. Some of the tests were centred on the validation of the drivers of sensors and actuators and were carried out over the flying model of the satellite. Others, more complex, constituted end-to-end tests where the concurrency of modules, the real-time control requirements and even the well-formedness of the telemetry data were verified. This work presents an incremental and highly automatised way for performing the ACS validation program based on two development suites and an end-to-end validation environment. The validation environment combines a Flat Satellite (FlatSat) configuration and a real-time emulator working in closed-loop. The FlatSat is built using the NS-1B Qualification Model (QM) hardware and it can run a complete version of the on-board software with the ACS modules fully integrated. The real-time emulator, running on an industrial PC, samples the actuation signals and emulates the sensors signals to close the control loop with the FlatSat. This validation environment constitutes a low-cost alternative to the classical three axes tilt table, with the advantage of being easily configured for working under specific orbit conditions, in accordance with any of the selected tests. The approach has been successfully applied to the NS-1B in order to verify different ACS modes under multiple orbit scenarios, providing an exhaustive coverage and reducing the risk of eventual errors during the satellite's lifetime. The strategy was applied also during the validation of the maintenance and reconfiguration procedures required once the satellite was launched. This paper describes in detail the complete ACS validation process that was performed and it shows the most relevant errors detected and fixed during testing. Finally it summarises some of the most significant conclusions. 相似文献
917.
《中国航空学报》2021,34(3):25-38
The attenuation of spatially evolving instability Tollmien-Schlichting (T-S) waves in the boundary layer of a flat plate with zero pressure gradients using an active feedback control scheme is theoretically and numerically investigated. The boundary layer is excited artificially by various perturbations to create a three-dimensional field of instability waves. Arrays of actuators and sensors are distributed locally at the wall surface and connected together via a feedback controller. The key elements of this feedback control are the determination of the dynamic model of the flat plate boundary layer between the actuators and the sensors, and the design of the model-based feedback controller. The dynamic model is established based on the linear stability calculation which simulates the three-dimensional input-output behaviour of the boundary layer. To simplify the control problem, an uncoupled control mode of the dynamic model is made to capture only those dynamics that have greatest influences on the input-output behaviour. A Proportional-Integral-Derivative (PID) controller, i.e. a lead-lag compensator, combining with a standard Smith predictor is designed based on the system stability criterion and the specifications using frequency-response methods. Good performance of the feedback control with the uncoupled control mode is demonstrated by the large reduction of the three-dimensional disturbances in the boundary layer. This simple feedback control is realistic and competitive in a practical implementation of T-S wave cancellation using a limited number of localised sensors and actuators. 相似文献
918.
文章从信息集成的角度提出四项一体化设计方法。制导与弹道的一体化设计,采用联立法实现用统一的架构解决复杂约束下飞行器自主动态轨迹规划问题。结果表明这种架构能够灵活处理各种约束条件并具有很高的控制精度,后续的重点是进一步提高计算效率。自检测BIT与地面测试的一体化设计,通过基于高速测量总线的窃听技术、基于模型和数据驱动的自动判读技术以及系统在回路的综合测试技术,实现快速发射和减少技术保障人员的目标,并已逐步开始应用。控制与测量系统的一体化设计,通过平台化的设计方案实现功能模块的集成、重用和重组,降低开发成本,避免重复投资。模型驱动的软硬件一体化设计,通过构建软硬件协同设计平台,实现算法、软件、硬件的并行设计和综合仿真,为系统方案的选择提供定量分析工具。上述信息集成技术为基础理论研究、系统实现和设计方法学等提供新的思路,提升控制系统的自主性和适应性,拓展控制系统的作用,增强快速反应能力,并能有效降低成本。 相似文献
919.
为在轨服务任务中实施对失控目标的安全逼近与对接,开展了服务航天器超近程逼近过程的动力学与控制研究。通过引入描述相对运动构型变化的期望相对位置矢量和位置误差矢量,推导了一种新颖的相对轨道误差动力学模型;考虑对接机构安装位置及安装误差,并结合相对姿态动力学模型,建立了逼近过程的相对姿态轨道耦合动力学模型;根据逼近路径约束条件,设计了逼近过程的期望相对位置矢量导引律;基于相对姿态轨道一体化耦合动力学模型,设计了考虑未知有界干扰的自适应时变滑模控制律并利用李雅普诺夫稳定性理论证明了闭环系统的全局稳定性。仿真结果表明,设计期望相对位置矢量导引律的方法能够实现逼近过程的相对运动构型变化控制,并且所设计的自适应时变滑模控制律具有较高的控制精度。 相似文献
920.