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1.
Using a novel space platform-based manipulator with slewing and deployable links, the paper addresses two issues of considerable importance: (a) How important is it to model flexibility of the system? (b) How many modes are needed to adequately represent the elastic character? Results suggest that the fundamental mode is able to capture physics of the response quite accurately. Due to its massive character, the platform dynamics is virtually unaffected, even by severe maneuvers of the manipulator. Hence, treating the platform as rigid would save the computational cost without affecting the accuracy. Although the link flexibility does affect the manipulator's tip vibration, the joint and platform vibrations remain negligible. The revolute joint flexibility appears to be an important parameter affecting both the joint as well as tip responses. The information should prove useful in the design of this new class of manipulators. 相似文献
2.
Sandro Da Silva Fernandes 《Acta Astronautica》1995,35(12):763-770
A complete first-order analytical solution is developed for the problem of optimum low-thrust limited power transfers between neighbouring elliptic non-equatorial orbits in a non-central gravity field. The optimization problem is formulated as a Mayer problem of optimal control with Cartesian elements as state variables. After applying the Pontryagin maximum principle and determining the optimal thrust acceleration, an intrinsic canonical transformation is performed: the Cartesian elements are changed by suitable orbital elements. Hori's method is applied in determining a first-order analytical solution. Simple analytical solutions are obtained explicitly for long-time transfers. 相似文献
3.
Darly Henriques da Silva 《Space Policy》2005,21(1):2098-63
The invitation to Brazil to join the International Space Station (ISS) program illustrates the way that foreign-policy makers in the USA favor short-term decisions over long-term commitments, while, in accepting the invitation, Brazil was also promoting other objectives. In taking the initiative to invite Brazil, President Clinton provided a unique opportunity to a middle-to-low-ranking spacefaring developing country to join the program as part of NASA's quota for the ISS. However, this action was the result of exchanges and bargains between the two countries, involving domestic and international interests on both sides—not all directly related to ISS activities—targeted at security and industrialization issues. These included the international non-proliferation regime, the commercialization of space systems and facilities (particularly Brazil's Alcantara Launch Center) and intellectual property. 相似文献
4.
Neri J. A. C. F. Dos Santos W. A. Rabay S. Fonseca I. M. De Souza P. N. Cividanes L. B. T. De Paula A. R. Oliveira Filho O. B. Almeida M. C. P. Francisco M. F. M. Varotto S. E. C. Ribeiro M. S. Saturno M. E. 《Acta Astronautica》1996,39(9-12):707-709
The National Space Research Institute (INPE) is developing the first Brazilian Scientific Microsatellite (SACI-1) based on the vanguard technology and on the experience acquired through projects developed by Brazilian Space Program. The SACI-1 is a 750km polar orbit satellite. The spacecraft will combine spin stabilization with geomagnetic control and has a total mass of 60 kg. The overall dimensions are 640×470×470 mm. The SACI-1 satellite shall be launched together with CBERS (China-Brazil Earth Resource Satellite). Its platform is being designed for multiple mission applications. The Brazilian Academy of Sciences has selected four scientific payloads that characterize the mission. The scientific experiments are: ORCAS (Solar and Anomalous Cosmic Rays Observation in the Magnetosphere), PLASMEX (Study of Plasma Bubbles), FOTSAT (Airglow Photometer), and MAGNEX (Geomagnetic Experiment). 相似文献
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航空公司运行控制中心是航空公司的核心,而飞行签派员又是运行控制中心的核心,运行控制中心的 效率直接影响到航空公司的运行安全与效益。根据航空公司飞行签派员的特点和管理现状,对效率量化和效 率评估进行分析研究,采用改进层次分析法(AHP)和物元可拓模型相结合的方法,建立适合我国航空公司飞 行签派员运行效率评估模型;针对评价指标在实际情况下更具有针对性和可操作性,提出4项准则和16项指 标组成的基于签派员航空公司运行效率评价指标体系,并进行算例分析。结果表明:所构建的评价指标体系合 理有效,能够真实反映出航空公司的运行效率与飞行签派员、运控设备、AOC组织结构与工作环境和航空公司 管理规定有着密切联系,为公司运行效率的提升提出理论依据。 相似文献
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在鸭式布局的基础上 ,对飞行器各部件及部件间的连接方式进行了外形隐身设计。对初步形成的鸭翼 -翼身融合体改变机身头部形状和立尾配置等进行 RCS优化。给出了飞行器各种状态下的 RCS平均值和迎头± 45°区内的 RCS值。测试结果表明 ,尖头机身、 30°双立尾 (立尾与垂直平面成± 30°角 )的鸭翼 -翼身融合体的 RCS值最小。对 RCS优化后的外形 ,风洞测力试验表明其气动性能也较好 (最大升阻比达到 8,失速迎角超过 2 6°) 相似文献
9.
A novel extended methodology for chatter suppression in milling process by applying external forced vibrations to the workpiece in two orthogonal directions which are the feed and cross-feed directions.Both the regenerative and forced chatter suppression during the milling process of flexible workpieces are investigated.Here,the workpiece is subject to a sinusoidal periodic force in the feed direction to disrupt the regenerative effect.Additionally,to minimize the forced chatter,the workpiece is subject to the periodic excitation force in cross-feed direction.This force is proportional to the magnitude of the estimated cutting force in cross-feed direction and has a phase opposite to the cutting force to minimize the vibration amplitudes.The effectiveness of the proposed method is evaluated numerically and experimentally,for the spindle speed located in both the local minima and local maxima of the stability lobe diagram.The numerical simulations indicate significant suppression effect in terms of vibration amplitudes,resulting in suppression of both the regenerative chatter and the forced chatter.Experiments were conducted by using a workpiece-mounted active stage composed of flexure hinges and driven by piezoelectric actuators.The experimental results agree qualitatively with the numerical simulations.The proposed method indicates a remarkable vibration reduction effect for both regenerative and forced chatters. 相似文献
10.
Heloísa Alves da Silva Paulo de Oliveira Camargo João Francisco Galera Monico Marcio Aquino Haroldo Antonio Marques Giorgiana De Franceschi Alan Dodson 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
Global Navigation Satellite Systems (GNSS), in particular the Global Positioning System (GPS), have been widely used for high accuracy geodetic positioning. The Least Squares functional models related to the GNSS observables have been more extensively studied than the corresponding stochastic models, given that the development of the latter is significantly more complex. As a result, a simplified stochastic model is often used in GNSS positioning, which assumes that all the GNSS observables are statistically independent and of the same quality, i.e. a similar variance is assigned indiscriminately to all of the measurements. However, the definition of the stochastic model may be approached from a more detailed perspective, considering specific effects affecting each observable individually, as for example the effects of ionospheric scintillation. These effects relate to phase and amplitude fluctuations in the satellites signals that occur due to diffraction on electron density irregularities in the ionosphere and are particularly relevant at equatorial and high latitude regions, especially during periods of high solar activity. As a consequence, degraded measurement quality and poorer positioning accuracy may result. 相似文献