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排序方式: 共有128条查询结果,搜索用时 78 毫秒
61.
Adams G.F. Ausherman D.A. Crippen S.L. Sos G.T. Williams B.P. Heidelbach R. 《Aerospace and Electronic Systems Magazine, IEEE》1996,11(12):31-35
The Environmental Research Institute of Michigan (ERIM) and Horizons, Inc. have completed the development, calibration and evaluation of the Advanced Research Projects Agency (ARPA)/US Army Topographic Engineering Center (TEC) funded IFSARE (Interferometric Synthetic Aperture Radar for Digital Terrain Elevations) system. This system rapidly produces geocoded SAR imagery and digital terrain elevation data. The dual-channel, X-band SAR is installed in the ERIM Learjet 36. The ground processor was developed in collaboration with the NASA Jet Propulsion Laboratory. The system produces 1.5 to 3.0 meters (1 sigma) absolute accuracy three-dimensional terrain elevation data over large areas without the use of ground control points. Several examples from recent data collections are presented 相似文献
62.
Experience at Harris with managing change through Continuous Improvement (CI) has demonstrated it is a Socio-Technical process... that is, the human elements are crucial and must be addressed before pressing for structural, institutional or technological change. Harris utilizes a five-stage business improvement model. It is not a road map to problem solving, rather it is an analysis and direction-setting framework, which can be applied to virtually any business situation. We have used it to insert major technology advances, characterize multifunctional business processes, solve a problem, develop a new product, improve a service, etc. The model is easy to teach, easy to understand, and easy to follow. It guides the application of the correct set of Continuous Improvement tools at the correct time to achieve the goal 相似文献
63.
Impact structures are a rare habitat on Earth. However, where they do occur they can potentially have an important influence on the local ecology. Some of the types of habitat created in the immediate post-impact environment are not specific to the impact phenomenon, such as hydrothermal systems and crater lakes that can be found, for instance, in post-volcanic environments, albeit with different thermal characteristics than those associated with impact. However, some of the habitats created are specifically linked to processes of impact processing. Two examples of how impact processing of target materials has created novel habitats that improve the opportunities for colonization are found in the Haughton impact structure in the Canadian High Arctic. Impact-shocked rocks have become a habitat for endolithic microorganisms, and large, impact-shattered blocks of rock are used as resting sites by avifauna. However, some materials produced by an impact, such as melt sheet rocks, can make craters more biologically depauperate than the area surrounding them. Although there are no recent craters with which to study immediate post-impact colonization, these data yield insights into generalized mechanisms of how impact processing can influence post-impact succession. Because impact events are one of a number of processes that can bring localized destruction to ecosystems, understanding the manner in which impact structures are recolonized is of ecological interest. Impact craters are a universal phenomenon on solid planetary surfaces, and so they are of potential biological relevance on other planetary surfaces, particularly Mars. 相似文献
64.
We identify a subsample of the recently detected extrasolar planets that is minimally affected by the selection effects of the Doppler detection method. With a simple analysis we quantify trends in the surface density of this subsample in the period-Msin(i) plane. A modest extrapolation of these trends puts Jupiter in the most densely occupied region of this parameter space, thus indicating that Jupiter is a typical massive planet rather than an outlier. Our analysis suggests that Jupiter is more typical than indicated by previous analyses. For example, instead of MJup mass exoplanets being twice as common as 2 MJup exoplanets, we find they are three times as common. 相似文献
65.
Hummels D.R. Adams C. Harms B.K. 《IEEE transactions on aerospace and electronic systems》1983,(6):871-883
A numerical method is described for predicting the detection probability performance of a pulse receiver which uses square-law detection. The method is useful for receivers where the ratio of RF bandwidth to video bandwidth is in the range from 2 to 40; a range where numerical results have previously been hard to obtain. A key feature of the approach is that it takes into account the actual filter transfer functions, pulse envelope shape, and pulse frequency. 相似文献
66.
Andrew S. Carten Charles F. Sindt 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1983,3(6):5-18
Long-duration scientific balloon flights using conventional ballasting methods to compensate for daily loss of lift suffer a severe payload weight penalty. Typically, the weight of the expendable ballast approaches or exceeds the weight of the balloon and payload. This paper examines the concept of correcting for degraded lift by “gas replenishment” techniques, that is, by replacing lost helium inflatant from an on-board dewar. Appropriate equations are developed and curves are presented which demonstrate the clear theoretical superiority of the replenishment method. Design problems associated with the dewars and heat exchangers required to implement the gas replenishment concept are also discussed in detail. A series of curves is presented in which net load, dewar weight and quantity of helium required are plotted for specific balloons and float altitudes as a function of daily loss rate. The lack of relevant heat exchange data in the literature is cited as an obstacle to immediate prototype development. 相似文献
67.
C. W. F. Everitt M. Adams W. Bencze S. Buchman B. Clarke J. W. Conklin D. B. DeBra M. Dolphin M. Heifetz D. Hipkins T. Holmes G. M. Keiser J. Kolodziejczak J. Li J. Lipa J. M. Lockhart J. C. Mester B. Muhlfelder Y. Ohshima B. W. Parkinson M. Salomon A. Silbergleit V. Solomonik K. Stahl M. Taber J. P. Turneaure S. Wang P. W. Worden Jr. 《Space Science Reviews》2009,148(1-4):53-69
This is the first of five connected papers detailing progress on the Gravity Probe B (GP-B) Relativity Mission. GP-B, launched 20 April 2004, is a landmark physics experiment in space to test two fundamental predictions of Einstein’s general relativity theory, the geodetic and frame-dragging effects, by means of cryogenic gyroscopes in Earth orbit. Data collection began 28 August 2004 and science operations were completed 29 September 2005. The data analysis has proven deeper than expected as a result of two mutually reinforcing complications in gyroscope performance: (1) a changing polhode path affecting the calibration of the gyroscope scale factor C g against the aberration of starlight and (2) two larger than expected manifestations of a Newtonian gyro torque due to patch potentials on the rotor and housing. In earlier papers, we reported two methods, ‘geometric’ and ‘algebraic’, for identifying and removing the first Newtonian effect (‘misalignment torque’), and also a preliminary method of treating the second (‘roll-polhode resonance torque’). Central to the progress in both torque modeling and C g determination has been an extended effort on “Trapped Flux Mapping” commenced in November 2006. A turning point came in August 2008 when it became possible to include a detailed history of the resonance torques into the computation. The East-West (frame-dragging) effect is now plainly visible in the processed data. The current statistical uncertainty from an analysis of 155 days of data is 5.4 marc-s/yr (~14% of the predicted effect), though it must be emphasized that this is a preliminary result requiring rigorous investigation of systematics by methods discussed in the accompanying paper by Muhlfelder et al. A covariance analysis incorporating models of the patch effect torques indicates that a 3–5% determination of frame-dragging is possible with more complete, computationally intensive data analysis. 相似文献
68.
Interplanetary transfer of photosynthesis: an experimental demonstration of a selective dispersal filter in planetary island biogeography 总被引:2,自引:0,他引:2
Cockell CS Brack A Wynn-Williams DD Baglioni P Brandstätter F Demets R Edwards HG Gronstal AL Kurat G Lee P Osinski GR Pearce DA Pillinger JM Roten CA Sancisi-Frey S 《Astrobiology》2007,7(1):1-9
We launched a cryptoendolithic habitat, made of a gneissic impactite inoculated with Chroococcidiopsis sp., into Earth orbit. After orbiting the Earth for 16 days, the rock entered the Earth's atmosphere and was recovered in Kazakhstan. The heat of entry ablated and heated the rock to a temperature well above the upper temperature limit for life to below the depth at which light levels are insufficient for photosynthetic organisms ( approximately 5 mm), thus killing all of its photosynthetic inhabitants. This experiment shows that atmospheric transit acts as a strong biogeographical dispersal filter to the interplanetary transfer of photosynthesis. Following atmospheric entry we found that a transparent, glassy fusion crust had formed on the outside of the rock. Re-inoculated Chroococcidiopsis grew preferentially under the fusion crust in the relatively unaltered gneiss beneath. Organisms under the fusion grew approximately twice as fast as the organisms on the control rock. Thus, the biologically destructive effects of atmospheric transit can generate entirely novel and improved endolithic habitats for organisms on the destination planetary body that survive the dispersal filter. The experiment advances our understanding of how island biogeography works on the interplanetary scale. 相似文献
69.
Oman Charles M. Shebilske Wayne L. Richards Jason T. Tubré Travis C. Beall Andrew C. Natapoff Alan 《Spatial Cognition & Computation》2000,2(4):355-372
Human orientation and spatial cognition partlydepends on our ability to remember sets ofvisual landmarks and imagine their relationshipto us from a different viewpoint. We normallymake large body rotations only about a singleaxis which is aligned with gravity. However,astronauts who try to recognize environmentsrotated in 3 dimensions report that theirterrestrial ability to imagine the relativeorientation of remembered landmarks does noteasily generalize. The ability of humansubjects to learn to mentally rotate a simplearray of six objects around them was studied in1-G laboratory experiments. Subjects weretested in a cubic chamber (n = 73) and aequivalent virtual environment (n = 24),analogous to the interior of a space stationnode module. A picture of an object waspresented at the center of each wall. Subjectshad to memorize the spatial relationships amongthe six objects and learn to predict thedirection to a specific object if their bodywere in a specified 3D orientation. Percentcorrect learning curves and response times weremeasured. Most subjects achieved high accuracyfrom a given viewpoint within 20 trials,regardless of roll orientation, and learned asecond view direction with equal or greaterease. Performance of the subject group thatused a head mounted display/head tracker wasqualitatively similar to that of the secondgroup tested in a physical node simulator. Body position with respect to gravity had asignificant but minor effect on performance ofeach group, suggesting that results may alsoapply to weightless situations. A correlationwas found between task performance measures andconventional paper-and-pencil tests of fieldindependence and 2&3 dimensional figurerotation ability. 相似文献
70.
In this paper, we describe a compact, low cost, fast turn-around-time technique used at the Air Force Research Laboratory to study hypervelocity debris impact effects on spacecraft structures and components. The technique described was used to study debris effects in the areas of: shock physics, debris-produced contamination, chemical analyses of the impact ejecta and debris initiated spacecraft discharge. Examples of research results obtained with the technique are presented and illustrate problems encountered in the field of space debris effects on spacecraft. 相似文献