全文获取类型
收费全文 | 3265篇 |
免费 | 452篇 |
国内免费 | 241篇 |
专业分类
航空 | 828篇 |
航天技术 | 1404篇 |
综合类 | 110篇 |
航天 | 1616篇 |
出版年
2024年 | 11篇 |
2023年 | 82篇 |
2022年 | 95篇 |
2021年 | 131篇 |
2020年 | 117篇 |
2019年 | 104篇 |
2018年 | 130篇 |
2017年 | 49篇 |
2016年 | 86篇 |
2015年 | 115篇 |
2014年 | 292篇 |
2013年 | 179篇 |
2012年 | 210篇 |
2011年 | 284篇 |
2010年 | 188篇 |
2009年 | 204篇 |
2008年 | 191篇 |
2007年 | 175篇 |
2006年 | 164篇 |
2005年 | 154篇 |
2004年 | 119篇 |
2003年 | 97篇 |
2002年 | 102篇 |
2001年 | 95篇 |
2000年 | 87篇 |
1999年 | 95篇 |
1998年 | 55篇 |
1997年 | 49篇 |
1996年 | 48篇 |
1995年 | 48篇 |
1994年 | 23篇 |
1993年 | 22篇 |
1992年 | 30篇 |
1991年 | 32篇 |
1990年 | 22篇 |
1989年 | 18篇 |
1988年 | 28篇 |
1987年 | 17篇 |
1986年 | 5篇 |
1985年 | 3篇 |
1984年 | 2篇 |
排序方式: 共有3958条查询结果,搜索用时 875 毫秒
931.
932.
《中国航空学报》2020,33(5):1494-1504
Adapter ring is a commonly used component in non-cooperative satellites, which has high strength and is suitable to be recognized and grasped by the space manipulator. During proximity operations, this circle feature may be occluded by the robot arm or limited field of view. Moreover, the captured images may be underexposed when there is not enough illumination. To address these problems, this paper presents a structured light vision system with three line lasers and a monocular camera. The lasers project lines onto the surface of the satellite, and six break points are formed along both sides of the adapter ring. A closed-form solution for real-time pose estimation is given using these break points. Then, a virtual structured light platform is constructed to simulate synthetic images of the target satellite. Compared with the predefined camera parameters and relative positions, the proposed method is demonstrated to be more effective, especially at a close distance. Besides, a physical space verification system is set up to prove the effectiveness and robustness of our method under different light conditions. Experimental results indicate that it is a practical and effective method for the pose measurement of on-orbit tasks. 相似文献
933.
934.
935.
We investigate the relation between nontrivial spatial concepts such as holes and string loops from a qualitative spatial reasoning perspective. In particular, we concentrate on a family of puzzles dealing with this kind of objects and explain how a loop formed in a string shows a similar behavior to a hole in an object, at least regarding the qualitative constraints it imposes on the solution of the puzzle. Unlike regular holes, however, we describe how string loops can be dynamically created and destroyed depending on the actions on the string. Furthermore, under a Knowledge Representation point of view, we provide a formalization that allows the different puzzle states to be described in terms of string crossings and loops, together with the actions that can be executed for a state transition and the complex effects they cause on the state representation. This implies the consideration of a formal representation of the side effects of actions that create or destroy string loops and the soundness of this representation with respect to the more general representation of string states in knot theory. 相似文献
936.
Effects of optical parameter measurement uncertainties and solar irradiance fluctuations on solar sailing 总被引:1,自引:0,他引:1
Lorenzo Niccolai Alessandro Anderlini Giovanni Mengali Alessandro A. Quarta 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(9):2784-2794
The heliocentric orbital dynamics of a spacecraft propelled by a solar sail is affected by some uncertainty sources, including possible inaccuracies in the measurement of the sail film optical properties. Moreover, the solar radiation pressure, which is responsible for the solar sail propulsive acceleration generation, is not time-constant and is subject to fluctuations that are basically unpredictable and superimposed to the well-known 11-year solar activity cycle. In this context, this work aims at investigating the effects of such uncertainties on the actual heliocentric trajectory of a solar sail by means of stochastic simulations performed with a generalized polynomial chaos procedure. The numerical results give an estimation of their impact on the actual heliocentric trajectory and identify whether some of the uncertainty sources are more relevant than others. This is a fundamental information for directing more accurate theoretical and experimental efforts toward the most important parameters, in order to obtain an accurate knowledge of the solar sail thrust vector characteristics and, eventually, of the spacecraft heliocentric position. 相似文献
937.
评价遥感图像的质量既可以采用客观的方法也可以采用主观的方法。重点研究了遥感图像质量主观评价方法。回顾了主观评价使用的量表法和任务满足度法的主要思想。由1∶500~1∶10 000比例尺制图的图示要求,概括出了若干个典型的满足一定规范要求的测绘业务,设计了一个心理物理试验,对这些测绘业务进行了研究,开发了一个面向1∶500~1∶10 000比例尺制图的主观图像质量评价标准。 相似文献
938.
Space robotics is regarded as one of the most impressing approaches for space debris removal missions. Due to the residual momentum of debris, it is essential to stabilize the base rapidly after capture. This paper presents a novel control strategy for stabilization of a space robot in postcapture considering actuator failures and bounded torques. In the control strategy, the motion of the manipulator is not regarded as a disturbance to the base; in contrast, it is utilized to compensate for the limitation of the control torques by means of an inverse dynamical model of the system. Different scenarios where actuators are external mechanisms or momentum exchange devices have been carried out, and for actuator failures, both single- and two-actuator failures have been considered. Regarding to the performance of actuators, control torques are bounded. In cases that either single or two actuators have failed, the base can be stabilized kinematically when actuators are external mechanisms, but can only be stabilized dynamically when only momentum exchange devices are used. Finally, a space robot with a seven-degree-of-freedom manipulator in postcapture is studied to verify the validity and feasibility of the proposed control scheme. Simulation results show that the whole system can be stabilized rapidly. 相似文献
939.
Peter M.B. Waswa Michael ElliotJeffrey A. Hoffman 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
Space missions designed to completely ablate upon an uncontrolled Earth atmosphere reentry are likely to be simpler and cheaper than those designed to execute controlled reentry. This is because mission risk (unavailability) stemming from controlled reentry subsystem failure(s) is essentially eliminated. NASA has not customarily implemented Design-for-Demise meticulously. NASA has rather approached Design-for-Demise in an ad hoc manner that fails to entrench Design-for-Demise as a mission design driver. Thus, enormous demisability challenges at later formulation stages of missions aspired to be demisable are evident due to these perpetuated oversights in entrenching Design-for-Demise practices. The investigators hence propose a strategy for a consistent integration of Design-for-Demise practices in all phases of a space mission lifecycle. Secondly, an all-inclusive risk-informed, decision-making methodology referred to as Analytic Deliberative Process is proposed. This criterion facilitates in making a choice between an uncontrolled reentry demisable or controlled reentry. The authors finally conceive and synthesize Objectives Hierarchy, Attributes, and Quantitative Performance Measures of the Analytical Deliberative Process for a Design-for-Demise risk-informed decision-making process. 相似文献
940.
Robert J. Ferl Agata Zupanska April Spinale David Reed Susan Manning-Roach George Guerra David R. Cox Anna-Lisa Paul 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
Molecular biology experiments on the International Space Station (ISS) continue to face challenges of sample harvesting and sample return to earth for post flight analysis; however, the use of Kennedy Space Center Fixation Tubes filled with RNALater has proven to be a robust solution to many of these challenges. While it is clear that one direction of future spaceflight experimentation may be towards enhanced on-orbit analytical capabilities, the rapid progress of earth-bound analytical capacity dictates that facile return of molecular biology samples from the ISS will continue to be a mainstay of space life sciences research and flight operations. In this paper we present a case study of the successful performance of KFTs and RNALater over a broad set of operational conditions of ascent configuration, on-orbit experiment use, on-orbit storage and sample return configurations that are unique to ISS current operations and constraints. We also provide observations on performance limits and discuss deployment opportunities and scenarios that are consistent with continued successful ISS molecular biology experimentation. 相似文献