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101.
A. Jäggi L. Prange U. Hugentobler 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
Gravity missions are equipped with onboard Global Positioning System (GPS) receivers for precise orbit determination (POD) and for the extraction of the long wavelength part of the Earth’s gravity field. As positions of low Earth orbiters (LEOs) may be determined from GPS measurements at each observation epoch by geometric means only, it is attractive to derive such kinematic positions in a first step and to use them in a second step as pseudo-observations for gravity field determination. The drawback of not directly using the original GPS measurements is, however, that kinematic positions are correlated due to the ambiguities in the GPS carrier phase observations, which in principle requires covariance information be taken into account. We use GRACE data to show that dynamic or reduced-dynamic orbit parameters are not optimally reconstructed from kinematic positions when only taking epoch-wise covariance information into account, but that essentially the same orbit quality can be achieved as when directly using the GPS measurements, if correlations in time are taken into account over sufficiently long intervals. For orbit reconstruction covariances have to be considered up to one revolution period to avoid ambiguity-induced variations of kinematic positions being erroneously interpreted as orbital variations. For gravity field recovery the advantage is, however, not very pronounced. 相似文献
102.
Much has been written in the last ten years about how the use of commercial-off-the-shelf (COTS) components would revolutionize the aerospace industry avionics, communication, navigation, surveillance/air traffic management (CNS/ATM) as well as global air traffic management (GATM). Civil aviation authorities around the world have been faced with numerous requests to certify aircraft containing increasing percentages of COTS components, much of it never designed or intended for use in the safety critical environment of an aircraft. Product service history is one method for demonstrating that such software is acceptable for use. In theory, product service history would seem to be a fairly simple concept, both to understand and to apply. However, in practice, such use has proven extremely problematic, as questions of how to measure the historic performance and the relevance of the provided data have surfaced. This paper elaborates a research effort funded by the United States Federal Aviation Administration to collect, analyze, and synthesize what is known and understood about applying product service history. The effort is limited to the topic of software product service history as applied in the certification of airborne systems and equipment. 相似文献
103.
Interplanetary outflows from coronal mass ejections (ICMEs) are structures shaped by their magnetic fields. Sometimes these
fields are highly ordered and reflect properties of the solar magnetic field. Field lines emerging in CMEs are presumably
connected to the Sun at both ends, but about half lose their connection at one end by the time they are observed in ICMEs.
All must eventually lose one connection in order to prevent a build-up of flux in the heliosphere; but since little change
is observed between 1 AU and 5 AU, this process may take months to years to complete. As ICMEs propagate out into the heliosphere,
they kinematically elongate in angular extent, expand from higher pressure within, distort owing to inhomogeneous solar wind
structure, and can compress the ambient solar wind, depending upon their relative speed. Their magnetic fields may reconnect
with solar wind fields or those of other ICMEs with which they interact, creating complicated signatures in spacecraft data. 相似文献
104.
C.R. Philbrick K.U. Grossmann R. Hennig G. Lange D. Offermann D. Krankowsky F.J. Schmidlin U. von Zahn 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1982,2(10):121-124
During the Energy Budget Campaign, several profiles of the density and temperature of the upper atmosphere were obtained. The measurements were made using rocket-borne instrumentation launched from ESRANGE, Sweden and Andoya Rocket Range, Norway during November and December, 1980. The techniques included meteorological temperature sondes, passive falling spheres, accelerometer instrumented falling spheres, density gauges, mass spectrometers and infrared emission experiments. The instruments provided data within the altitude range from 20 km to 150 km. The measurements were made during periods which have been grouped into three categories by level of geomagnetic activity. Analysis has been made to compare the results and to examine the oscillations and fluctuations in the vertical profiles for scales ranging between hundreds of meters and tens of kilometers. Most of the features observed fit qualitatively within the range expected for internal gravity waves. The geomagnetic storm conditions may be associated with enhanced wave activity and heating observed in the lower thermosphere. 相似文献
105.
We review the mechanisms which have been proposed for the heating of stellar chromospheres and coronae. These consist of heating by acoustic waves, by slow and fast mhd waves, by body and surface Alfvén waves, by current or magnetic field dissipation, by microflare heating and by heating due to bulk flows and magnetic flux emergence. Some relevant observational evidence has also been discussed. 相似文献
106.
The unique characteristics of the Space Station are changing the ways payloads are designed and accommodated for orbital flight. Station accommodations need to be versatile and operationally flexible to permit integration of many types of equipment in a variety of modes; and autonomous to render each payload independent or invisible to the rest of the system and other mission equipment. This paper presents the various categories of Space Station payloads, the user facilities that are being designed to accommodate them, illustrates through scientific and commercial scenarios the utilization of those facilities, and identifies the factors that must be considered to make the Space Station an effective tool for the users. 相似文献
107.
Mende S.B. Frey H.U. Immel T.J. Gerard J.-C. Hubert B. Fuselier S.A. 《Space Science Reviews》2003,109(1-4):211-254
The IMAGE spacecraft carries three FUV photon imagers, the Wideband Imaging Camera (WIC) and two channels, SI-12 and SI-13, of the Spectrographic Imager. These provide simultaneous global images, which can be interpreted in terms of the precipitating particle types (protons and electrons) and their energies. IMAGE FUV is the first space-borne global imager that can provide instantaneous global images of the proton precipitation. At times a bright auroral spot, rich in proton precipitation, is observed on the dayside, several degrees poleward of the auroral zone. The spot was identified as the footprint of the merging region of the cusp that is located on lobe field lines when IMF Bz was northward. This identification was based on compelling statistical evidence showing that the appearance and location of the spot is consistent with the IMF Bz and By directions. The intensity of the spot is well correlated with the solar wind dynamic pressure and it was found that the direct entry of solar wind particles could account for the intensity of the observed spot without the need for any additional acceleration. Another discovery was the observation of dayside sub-auroral proton arcs. These arcs were observed in the midday to afternoon MLT sector. Conjugate satellite observations showed that these arcs were generated by pure proton precipitation. Nightside auroras and their relationship to substorm phases were studied through single case studies and in a superimposed epoch analysis. It was found that generally there is substantial proton precipitation prior to substorms and the proton intensity only doubles at substorm onset while the electron auroral brightness increases on average by a factor of 5 and sometimes by as much as a factor of 10. Substorm onset occurs in the central region of the pre-existing proton precipitation. Assuming that nightside protons are precipitating from a quasi-stable ring current at its outer regions where the field lines are distorted by neutral sheet currents we can associate the onset location with this region of closed but distorted field lines relatively close to the earth. Our results also show that protons are present in the initial poleward substorm expansion however later they are over taken by the electrons. We also find that the intensity of the substorms as quantified by the intensity of the post onset electron precipitation is correlated with the intensity of the proton precipitation prior to the substorms, highlighting the role of the pre-existing near earth plasma in the production of the next substorm. 相似文献
108.
We review some aspects of low latitudes (L≤2) geomagnetic field variations associated with magnetospheric pulsations as well
as with continuous and impulsive variations of the solar wind (SW) pressure.
This revised version was published online in August 2006 with corrections to the Cover Date. 相似文献
109.
There is renewed interest in using nuclear power in a variety of ways in space, as well as in disposing of terrestrial nuclear waste aloft. While the benefits of such use to space exploration might be high, the potential costs to Earth and its inhabitants are currently too dear. Accidents have already occurred which, despite official denials, have spread radiation worldwide. Such denials are characteristic of the closed and secretive nature of the nuclear ‘debate’. This viewpoint calls for the involvement of all those concerned with space nuclear power—lay, professional, government and NGO—in decisions on whether to proceed with it and suggests that maybe we should wait for safer scientific discoveries before we attempt further planetary exploration. 相似文献
110.
Bozzi S. Capigatti U. Cappellini V. Re E.D. Margheri M. Saltini I. 《IEEE transactions on aerospace and electronic systems》1982,(5):704-708
The design and implementation of a second-order nonrecursive moving target indication (MTI) radar filter using commercially available charge-transfer devices as delay lines are described. A simple technique is included to compensate for the device charge-transfer in-efficiency and its sensitivity is analyzed. Experimental laboratory tests and results in an operating radar system are reported showing the good performance of the realized MTI radar filter. 相似文献