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201.
A method is presented for reducing trajectory sensitivity and achieving robust asymptotic tracking for linear feedback systems when there are parameter perturbations and disturbance inputs. The controller consists of a servocompensator containing the modes of the reference signals and disturbance inputs, a stabilizing feedback loop, and a feedforward compensator. Application of the method to the design of a vertical takeoff and landing (VTOL) aircraft flight control system is discussed. The use of a precompensator allows performance maneuvers such that the aircraft tracks desired trajectories and the feedforward and feedback signals aid in reducing the trajectory sensitivity to variations of parameters due to change in airspeed and to wind gust. Simulation results are presented to show the robust tracking, disturbance rejection, and sensitivity reduction capabilities of the flight control system. 相似文献
202.
R.D. Gehrz E.E. Becklin I. de Pater D.F. Lester T.L. Roellig C.E. Woodward 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2009
The Stratospheric Observatory for Infrared Astronomy (SOFIA) is a joint US/German Project to develop and operate a gyrostabilized 2.5-m telescope in a Boeing 747-SP. This observatory will allow astronomical observations from 0.3 μm to sub-millimeter wavelengths at stratospheric altitudes as high as 45,000 ft where the atmosphere is not only cloud-free, but largely transparent at infrared wavelengths. The dynamics and chemistry of interstellar matter, and the details of embedded star formation will be key science goals. In addition, SOFIA’s unique portability will enable large-telescope observations at sites required to observe transient phenomena and location specific events. SOFIA will offer the convenient accessibility of a ground-based telescope for servicing, maintenance, and regular technology upgrades, yet will also have many of the performance advantages of a space-based telescope. Initially, SOFIA will fly with nine first-generation focal plane instruments that include broad-band imagers, moderate resolution spectrographs that will resolve broad features from dust and large molecules, and high resolution spectrometers capable of studying the chemistry and detailed kinematics of molecular and atomic gas. First science flights will begin in 2010, leading to a full operations schedule of about 120 8–10 h flights per year by 2014. The next call for instrument development that can respond to scientifically exciting new technologies will be issued in 2010. We describe the SOFIA facility and outline the opportunities for observations by the general scientific community with cutting edge focal plane technology. We summarize the operational characteristics of the first-generation instruments and give specific examples of the types of fundamental scientific studies these instruments are expected to make. 相似文献
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H.S. Sawant J.R. Cecatto H. Mészárosová C. Faria F.C.R. Fernandes M. Karlický M.C. de Andrade 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2009
The digital, decimetric (950–2500 MHz) Brazilian Solar Spectroscope (BSS, Sawant, H.S., Subramanian, K.R., Faria, C., et al. Brazilian Solar Spectroscope (BSS). Solar Phys. 200, 167–176, 2001) with high time (10–1000 ms) and frequency (1–10 MHz) resolution is in regular operation since April, 1998, at the National Space Research Institute (INPE) at São José dos Campos, Brazil. The BSS has now been upgraded with a new digital data acquisition and data processing system. The new version of the BSS has improved the observational possibilities with the capability to record up to 200 frequency channels available in the selectable frequency range 950–2500 MHz. The GPS receiver permits the acquisition of data with time accuracy in the order of 0.1 ms. The software system of the BSS is composed by two distinct modules: the first, data acquisition system provides a flexible Graphical User Interface (GUI) that allows one to choose the observational parameters. The second module is the real time visualization system that permits real time visualization of the observed dynamic spectrum and additionally allows procedures for visualization and preliminary analysis of the recorded solar spectra. Using the new visualization system, we have realized two new types of dm-radio fine structures: narrow band type III bursts with positive as well as negative group frequency drift and dots emissions arranged in zebra-like and fiber-like chains. Furthermore, we have found flare generated fast wave trains according to their tadpole signature in wavelet power spectra for a decimetric type IV radio event (June 6, 2000 flare). 相似文献
206.
基于传动误差设计的弧齿锥齿轮啮合分析 总被引:34,自引:2,他引:34
提出了基于传动误差设计的弧齿锥齿轮啮合质量控制的新概念。首先分析了传动误差所反映的弧齿锥齿轮传动的动态特性、强度性能等众多信息,包括设计重合度、实际重合度、振动激励、边缘接触、载荷齿间分配和齿面印痕相对于误差的敏感性。在此基础上,提出了高重合度传动误差曲线的设计,通过齿面接触路径方向的倾斜,重合度能够高至 2.0~ 3.0,有效地改善了齿轮动态特性,提高了强度。进一步又提出了几何传动误差曲线幅值的设计,结合承载传动误差,使齿轮在不同载荷条件下既能具有高的重合度,又保证了相对低的误差敏感性。其后提出的四阶传动误差曲线的设计,除上述优点外,还改进了齿轮的轻载振动和噪声。最后论述了基于传动误差设计的弧齿锥齿轮的相应制造方法。该研究为高性能弧齿锥齿轮的开发开辟了途径。 相似文献
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208.
美国航空推进系统关键技术 总被引:3,自引:0,他引:3
方昌德 《燃气涡轮试验与研究》2001,14(3):1-6
在美国的国防关键技术计划中,航空推进技术受到重视。通过对美国国家级计划--高性能涡轮发动机综合技术计划、脉冲式爆震波产生推力的新概念发动机计划、燃烧室内气流过渡为超声速的冲压发动机计划的研究,对美国选择推进系统的理由作了分析,并对各国在航空推进系统的研究和发展工作进行了评估。可以看出,日本、德国继美、英、法、俄后在航空航天的推进系统方面已完成了一系列的研究。日本斥巨资建立发动机模拟高空试验台。最后详细列出了燃气涡轮发动机,其它航空动力和燃料三类中的10项关键技术。 相似文献
209.
P. S. Thé L. Matveyenko J. Kleczek L. M. Gindilis G. M. Rudnitskij J. Arbocz J. Schuve J. A. Steketee W. de Graaff K. A. van der Hucht Wayne G. Roberge G. Kockarts R. H. van Gent E. Dekker T. S. van Albada D. de Hoop H. Nieuwenhuijzen Josip Kleczek J. L. van Ingen P. Hellings A. Achterberg 《Space Science Reviews》1985,41(1-2):201-213
210.
Kleczek J. van Gent R. H. Rutten Robert J. de Munck J. C. Slottje C. Severne G. Pecker Jean-Claude Postma H. Grishchuk L. P. Niewenhuijzen H. Schuiling R. D. van Beek H. F. Reijnen G. C. M. Heidmann Jean Lemaire J. Bleeker Johan Icke V. Neéman Y. Feast M. W. de Graaff W. 《Space Science Reviews》1986,43(3-4):383-396
Space Science Reviews - 相似文献