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1.
The paper aims at giving a few methodological suggestions in deterministic earthquake prediction studies based on combined ground-based and space observations of earthquake precursors. Up to now what is lacking is the demonstration of a causal relationship with explained physical processes and looking for a correlation between data gathered simultaneously and continuously by space observations and ground-based measurements. Coordinated space and ground-based observations imply available test sites on the Earth surface to correlate ground data, collected by appropriate networks of instruments, with space ones detected on board of LEO satellites. At this purpose a new result reported in the paper is an original and specific space mission project (ESPERIA) and two instruments of its payload. The ESPERIA space project has been performed for the Italian Space Agency and three ESPERIA instruments (ARINA and LAZIO particle detectors, and EGLE search-coil magnetometer) have been built and tested in space. The EGLE experiment started last April 15, 2005 on board the ISS, within the ENEIDE mission. The launch of ARINA occurred on June 15, 2006, on board the RESURS DK-1 Russian LEO satellite. As an introduction and justification to these experiments the paper clarifies some basic concepts and critical methodological aspects concerning deterministic and statistic approaches and their use in earthquake prediction. We also take the liberty of giving the scientific community a few critical hints based on our personal experience in the field and propose a joint study devoted to earthquake prediction and warning. 相似文献
2.
重力卫星五年运行对求定地球重力场模型的进展和展望 总被引：3，自引：0，他引：3
对近年升空的CHAMP和GRACE和将于2007年升空的GOCE卫星在测定地球重力场方面的技术特点和初步成果进行了回顾、比较和评估。并对它们今后在静态和动态的地球重力场构模方面可能的进展作一展望。现在只用一颗重力卫星的轨道摄动数据，就可以以前所未有的可靠性和精确性来求定地球重力场的长波和部分中波。如CHAMP重力卫星的33个月数据所求定的地球重力场模型，相对于曾利用多颗卫星资料所推算的GRlM5-S1重力场模型，在长波方面的精度和可靠性都有很大改善。而GRACE重力卫星的110天数据所导出成果的空间分辨率，又优于CHAMP的33个月的数据成果。GRACE卫星还有一个重要任务，就是测定重力场非潮汐的短期性或准实时的变化。还介绍了新发表的一个联合地球重力场模型EIGEN-CG03C，360完全阶次，分辨率约30′。CG03C同CHAMP／GRACE以前的重力场模型比较，在400km波长的精度方面改善了一个量级，大地水准面的精度改善了3cm，重力异常的精度改善了0．4mgal。 相似文献
3.
对近年升空的CHAMP和GRACE和将于2007年升空的GOCE卫星在测定地球重力场方面的技术特点和初步成果进行了回顾、比较和评估。并对它们今后在静态和动态的地球重力场构模方面可能的进展作一展望。现在只用一颗重力卫星的轨道摄动数据，就可以以前所未有的可靠性和精确性来求定地球重力场的长波和部分中波。如CHAMP重力卫星的33个月数据所求定的地球重力场模型,相对于曾利用多颗卫星资料所推算的GR1M5 S1重力场模型,在长波方面的精度和可靠性都有很大改善。而GRACE重力卫星的 110天数据所导出成果的空间分辨率，又优于CHAMP的33个月的数据成果。GRACE卫星还有一个重要任务，就是测定重力场非潮汐的短期性或准实时的变化。还介绍了新发表的一个联合地球重力场模型EIGEN CG03C, 360完全阶次，分辨率约30′。CG03C同CHAMP/GRACE以前的重力场模型比较，在400 km波长的精度方面改善了一个量级，大地水准面的精度改善了3 cm，重力异常的精度改善了0.4 mgal。 相似文献
4.
Launch strategy for Indian lunar mission and precision injection to the Moon using genetic algorithm
V. Adimurthy R. V. Ramanan S. R. Tandon C. Ravikumar 《Journal of Earth System Science》2005,114(6):711-716
The Indian lunar mission Chandrayaan-1 will have a mass of 523 kg in a 100 km circular polar orbit around the Moon. The main
factors that dictate the design of the Indian Moon mission are to use the present capability of launch vehicles and to achieve
the scientific objectives in the minimum development time and cost. The detailed mission planning involves trade-off studies
in payload optimization and the transfer trajectory determination that accomplishes these requirements. Recent studies indicate
that for an optimal use of the existing launch vehicle and space-craft systems, highly elliptical inclined orbits are preferable.
This indeed is true for the Indian Moon mission Chandrayaan-1. The proposed launch scenario of the Indian Moon mission program
and capabilities of this mission are described in this paper, highlighting the design challenges and innovations. Further,
to reach the target accurately, appropriate initial transfer trajectory characteristics must be chosen. A numerical search
for the initial conditions combined with numerical integration produces the near accurate solution for this problem. The design
of such transfer trajectories is discussed in this paper. 相似文献
5.
一种人工影响天气微型无人驾驶飞机及初步试验 总被引：5，自引：0，他引：5
人工影响天气微型无人驾驶飞机用于复杂天气下人影作业，是可控和可回收探测器和播撒器。人工影响天气微型无人驾驶飞机系统由微型飞机、任务载荷（机载撒播装置和探测装置）及地面监视控制三部分构成。飞行前通过计算机给飞机上的机载控制系统设置航线,遥控起飞后可由机载控制系统控制,飞机按照预定航线进行自主飞行。在需要修改飞行方向时，也可通过遥控终端发出指令。在到达作业高度后，通过遥控终端发出指令，飞机开始播撒作业。在整个飞行过程中飞机不断探测大气温压湿和风，连续将探测资料和飞行数据发送给地面监视终端。通过试验验证了人工影响天气微型无人驾驶飞机飞行性能和探测能力：能够在携带1 kg播撒剂的情况下，飞达6 km的高度，作业半径20 km；能在雨天进行播撒作业和探测；飞机采用手掷起飞，对起飞的场地几乎没有要求；采用降落伞降落，可选择草地、农田降落。初步分析了对对流降水和雷电天气的适应能力。 相似文献
6.
Alain Dabas 《Comptes Rendus Geoscience》2010,342(4-5):370-379
Among the basic variables that characterize the thermodynamic state of the atmosphere, wind is relatively poorly observed. Surface measurements by in situ sensors are numerous, but irregularly distributed over the globe. Upper level winds are characterized by radiosoundings that are reliable and accurate, but in a very limited number due to their expensive cost. They are complemented by wind measurements performed by commercial aircrafts, but these data are mostly acquired along the major flight routes at a cruising altitude of ～10 km. Radio sondes and aircrafts leave large gaps in the observation network that have been partly complemented for 10 years by an increasing amount of wind information derived from cloud tracking in satellite images, and more recently, surface winds by scatterometers. However, the observation capacity still suffers deficiencies as there is still no information in cloud-free parts of the atmosphere, and no complete vertical profiles except for the radiosoundings. They should be overcome with the launch in 2011 of the European satellite ADM-Aeolus, a space-based Doppler lidar currently under development at the European Space Agency. 相似文献
7.
通过现场标准贯入试验,对国道317线K205+700～K207+100段路基填方段中的淤泥质粉细砂层进行了液化判别.<公路工程抗震设计规范>(JTJ004-89)和<建筑抗震设计规范>(GB5001-2001)的计算结果均表明该砂层会产生液化.但前一规范的计算值偏大,在工程中建议使用后一规范,并以振冲密实法进行预防. 相似文献
8.
The mathematical structure and numerical analysis of classical small deformation elasto–plasticity is generally well established. However, development of large deformation elastic–plastic numerical formulation for dilatant, pressure sensitive material models is still a research area. In this paper we present development of the finite element formulation and implementation for large deformation, elastic–plastic analysis of geomaterials. Our developments are based on the multiplicative decomposition of the deformation gradient into elastic and plastic parts. A consistent linearization of the right deformation tensor together with the Newton method at the constitutive and global levels leads toward an efficient and robust numerical algorithm. The presented numerical formulation is capable of accurately modelling dilatant, pressure sensitive isotropic and anisotropic geomaterials subjected to large deformations. In particular, the formulation is capable of simulating the behaviour of geomaterials in which eigentriads of stress and strain do not coincide during the loading process. The algorithm is tested in conjunction with the novel hyperelasto–plastic model termed the B material model, which is a single surface (single yield surface, affine single ultimate surface and affine single potential surface) model for dilatant, pressure sensitive, hardening and softening geomaterials. It is specifically developed to model large deformation hyperelasto–plastic problems in geomechanics. We present an application of this formulation to numerical analysis of low confinement tests on cohesionless granular soil specimens recently performed in a SPACEHAB module aboard the Space Shuttle during the STS‐89 mission. We compare numerical modelling with test results and show the significance of added confinement by the thin hyperelastic latex membrane undergoing large stretching. Copyright © 2001 John Wiley & Sons, Ltd. 相似文献
9.
The Moon 35 years after Apollo: What's left to learn? 总被引：1，自引：0，他引：1
Clive R. Neal 《Chemie der Erde / Geochemistry》2009,69(1):3-48
With the cancellation of the Apollo program after Apollo 17 returned from the Moon in 1972, the focus of NASA switched to other areas of the Solar System. Study of the Moon did continue through analysis of the returned samples and remotely sensed data sets (both orbital and surface), as well as through Earth-based telescopic studies. In the 1990s, new orbital data were obtained from several missions (fly-by and orbital), the first being Galileo that allowed the lunar farside to be mapped, followed by global mapping by the Clementine and Lunar Prospector missions.Interest in the Moon started to increase at the beginning of the 21st century as other nations focused their space exploration programs on the Moon. The speech by President Bush in January 2004 put the Moon back into the critical exploration path for NASA, paving the way for humans to return to the lunar surface by 2020. This return will be critical for developing technologies and protocols for the eventual human exploration of other parts of the solar system. At the time of writing (June 2008), the SELENE/Kaguya mission (Japan and Chang’e-1 (China) are orbiting the Moon, with Chandrayaan-1 (India) and Lunar Reconnaissance Orbiter (USA) being scheduled to launch later in 2008.The past (and present) exploration of the Moon begs the question “what's left to be done?” With the renewed focus on the Moon, now that it is on the pathway for the exploration of Mars (and beyond) a similar question has been raised - what should the astronauts do on the Moon? The publication of the New Views of the Moon book [Jolliff et al., 2006. New Views of the Moon, Reviews in Mineralogy, vol. 60. American Mineralogical Society, 721pp] highlighted a number of important scientific questions that remain unanswered as well as posing many more on the basis of the currently available data. These questions resonated in three Lunar Exploration Analysis Group (LEAG) reports pertinent to this discussion, which were also published (on line) during 2006 (http://www.lpi.usra.edu/leag), and in the National Research Council of the National Academies [2007. The Scientific Context for Exploration of the Moon. National Academies Press, Washington, DC, 112pp] report entitled “The Scientific Context for Exploration of the Moon”. This paper synthesizes these recent studies, along with those from the 1980s and 1990s, to emphasize the lunar science questions that remain unanswered. In addition, it summarizes the missions already flown to the Moon along with those that are planned in order to give the reader an idea of exactly what lunar science has been and will be conducted in the hope that it will inspire proposals for missions to address the outstanding science questions. 相似文献
10.
David J. Delene 《Earth Science Informatics》2011,4(1):29-44
The practice of conducting quality control and quality assurance in the construction of data sets is often an overlooked and
underestimated task of many research projects in the Earth Sciences. The development of software to effectively process and
quickly analyze measurements is a critical aspect of a research project. An evolutionary approach has been used at the University
of North Dakota to develop and implement software to process and analyze airborne measurements. Development over the past
eight years has resulted in a collection of software named the Airborne Data Processing and Analysis (ADPAA) package which
has been published as an open source project on Source Forge. The ADPAA package is intended to fully automate data processing
while incorporating the concept of missing value codes and levels of data processing. At each data level, ADPAA utilizes a
standard ASCII file format to store measurements from individual instruments into separate files. After all data levels have
been processed, a summary file containing parameters of scientific interest for the field project is created for each aircraft
flight. All project information is organized into a standard directory structure. ADPAA contains several tools that facilitate
quality control procedures conducted on instruments during field projects and laboratory testing. Each quality control procedure
is designed to ensure proper instrument performance and hence the validity of the instrument’s measurement. Data processing
by ADPAA allows edit files to be created that are automatically used to insert missing value codes into a time period that
had instrument problems. The creation of edit files is typically done after the completion of a field project when scientists
are performing quality assurance of the data set. Since data processing is automatic, preliminary data can be created and
analyzed within hours of an aircraft flight and a complete field project data set can be reprocessed many times during the
quality assurance process. Once a final data set has been created, ADPAA provides several tools for visualization and analysis.
In addition to aircraft data, ADPAA can be used on any data set that is based on time series measurements. The concepts illustrated
by ADPAA and components of ADPAA, such as the Cplot visualization tool, are applicable to areas of Earth Science that work
with time series measurements. 相似文献
11.
The Arizona Department of Transportation (ADOT) is preparing to upgrade State Route 260 between Payson and Heber. It is estimated that a total of about one million cubic meters of water will be required for embankment construction during a period of about 84 months to upgrade the first 33.8 km of the highway. ADOT is investigating various sources of construction water for use in the highway improvement project, including groundwater resources along the highway corridor. A region known as the RV site, underlain by fractured granite, is located 12.9 km east of Payson. The site includes three springs, a creek and several wells. Several boreholes and observation wells were made to a maximum depth of 157 m to obtain fracture data and to conduct pumping tests with monitoring. Fracture data recorded by acoustic televiewer logs were used to build a fracture network model for the rock mass. Results of a 24-hour and a 7-day pumping tests were used to calibrate hydraulic parameters of a finite element discrete fracture fluid flow model considering the region as a heterogeneous, anisotropic, fractured medium. A 38-day multi-well pumping test was used to validate the calibrated numerical model. The calibrated model showed the capability to provide reasonably accurate predictions for new pumping tests conducted in the same well field. The validated model was then used to simulate pumping exceeding a 7 year period under different scenarios incorporating different sets of boundary conditions and different pumping rates at multi-wells, with and without recharge, to evaluate the yield of the aquifer and to assess the effect of long-term pumping on the environment. The results indicated that (a) the combined yield of the wells in the RV site is sufficient to meet the water demand for the ADOT highway project and (b) the water levels in the well field would decline between 3.0 and 7.6 m after one year of pumping and by 12.2 to over 30.5 m during the life of the project. 相似文献
12.
固结与流变特性及其参数取值研究是软基上结构物长期沉降课题的重要组成部分。针对宁波轨道交通工程的两个典型土层,开展了基于GDS固结仪的流变固结试验,获得了土样的主固结与次固结性状参数。采用Gibson三元件流变模型结合Matlab软件的拟合功能,得到了土样的三元件流变模型参数。通过对试验结果进行分析总结,发现宁波软土的次固结过程表现出较明显的非线性。次固结系数Ca与压缩指数Cc近似符合 Ca/Cc=0.02±0.01。宁波软土的一维流变过程符合Gibson三元件流变模型规律,且其模量参数和黏滞系数均随固结压力的增大而增大。 相似文献
13.
D. Bala Subrahamanyam Radhika Ramachandran S. Indira Rani S. Sijikumar T. J. Anurose Asish Kumar Ghosh 《Natural Hazards》2012,61(3):893-910
Accurate knowledge of different meteorological parameters over a launch site is very crucial for efficient management of satellite
launch operations. Local weather over the Indian satellite launch site located at Sriharikota High Altitude Range (SHAR: 13.72°N,
80.22°E) is very much dependent on the atmospheric circulation prevailing over the Bay of Bengal oceanic region and topography-induced
convective activities. With a view to providing severe weather threat prediction in terms of launch commit criteria (LCC),
two numerical atmospheric models namely high-resolution regional model (HRM) and advanced regional prediction system (ARPS)
are made operational over SHAR in a synoptic and mesoscale domain, respectively. In the present research article, two launch
campaigns through Polar Satellite Launch Vehicle (PSLV-C11 and PSLV-C12) when contrasting weather conditions prevailed over
the launch site are chosen for demonstration of potential of two models in providing location-specific short-to-medium-range
weather predictions meeting the needs of LCC. In the case of PSLV-C11 campaign, when the launch site underwent frequent thundershower-associated
rainfall, ARPS model–derived meteorological fields were effectively used in prediction of probability of the wet spells. On
the other hand, Bay of Bengal underwent severe cyclonic storm during PSLV-C12 campaign, and its formation was reasonable captured
through HRM simulations. It is concluded that a combination of HRM and ARPS provide reliable short-to-medium-range weather
prediction over SHAR, which has got profound importance in launch-related activities. 相似文献
14.
硬化土（hardening soil）模型是岩土工程数值分析中常采用的模型。为研究加载方式和排水条件对原状花岗岩残积土剪切行为的影响,对深圳地区原状花岗岩残积土进行了常规三轴固结排水、常规三轴固结不排水、固结排水侧向卸载和固结不排水侧向卸载4组试验,并由试验结果确定出不同加载方式和排水条件下的硬化土模型参数。结果表明：在常规三轴试验中,试样在剪切过程中表现为先剪缩后剪胀的特性,在侧向卸载试验中,试样始终表现为剪胀的特性;模型参数值与加载路径密切相关,固结不排水侧向卸载试验（CDLU）测得的有效内摩擦角 较常规三轴固结不排水试验（CD）试验大20%,而有效黏聚力 小了46%;CDLU试验得到的三轴压缩试验的参考割线模量 为CD试验的2.9倍,卸载再加载参考割线模量 为CD试验的1.8倍;在相同加载路径下,模型参数值也受排水条件的影响,由CU试验得到的 与CD试验的结果相近,但CU试验得到的 要明显大于CD试验的结果,CU试验得到的 为CD试验的2倍, 为CD试验的3.8倍。因此,在岩土工程数值分析中应根据工程的实际情况确定和选用模型参数值。 相似文献
15.
M. B. Potdar S. A. Sharma V. Y. Parikh P. C. S. Devara P. E. Raj Y. K. Tiwari R. S. Maheskumar K. K. Dani S. K. Saha S. M. Sonbawne Y. Jaya Rao G. Pandithurai 《Journal of Earth System Science》2004,113(1):103-116
With the launch of the German Aerospace Agency's (DLR) Modular Opto-electronic Scanner (MOS) sensor on board the Indian Remote
Sensing satellite (IRS-P3) launched by the Indian Space Research Organization (ISRO) in March 1996, 13 channel multi-spectral
data in the range of 408 to 1010 nm at high radiometric resolution, precision, and with narrow spectral bands have been available
for a variety of land, atmospheric and oceanic studies. We found that these data are best for validation of radiative transfer
model and the corresponding code developed by one of the authors at Space Applications Centre, and called ATMRAD (abbreviated
for ATMospheric RADiation). Once this model/code is validated, it can be used for retrieving information on tropospheric aerosols
over ocean or land. This paper deals with two clear objectives, viz.,
The data validation procedure essentially involves
The results show that the model performance is satisfactory and a relationship between the spectral parameters of MOS radiances
and aerosol optical thickness can be established. In this communication, we present the details of the experiments conducted,
database, validation of the ATMRAD model and development of the relationship between AOT and MOS radiance. 相似文献
| 1 | Validation of ATMRAD model/code using MOS data and synchronously measured atmospheric data, and if found performing well, then to |
| 2 | derive relationship between MOS radiances and Aerosol Optical Thickness (AOT). |
| – | •near-synchronous measurements of columnar aerosol optical thickness and altitude profiles of aerosol concentration using ground-based multi-filter solar radiometers and Argon-ion Lidar, respectively and |
| – | •computation of the top-of-the-atmosphere (TOA) radiances from a low reflecting target (near clear water reservoir in the present study) using the ATMRAD model. |
16.
Design and Implementation of Space Dust Database 总被引：2，自引：0，他引：2
Space debris is very dangerous to the security of on-the-orbit spacecrafts, and it is increasing in number at high speed with the expansion of human space exploration. Space debris has become a serious space pollutant noticed by many astronomers. The increase of space dust sources and the development of research on space dust urgently need space dust data sharing and exchanging. It is necessary for us to establish the Space Dust Database to realize the sharing and canonical management of the data. The Space Dust Database (SDD) management system,based on the 3-layer B/S computer mode, was designed and implemented in this paper. The system‘s features include significantly improved runtime efficiency, good scalability and maintainability. The Space Dust Database can pTovide some scientific bases for the study of the chemical constituents, mineral composition, origin and sources of space dust, but also provide excellent data services and decision-making support for the protection of space and model construction of space dust. 相似文献
17.
Robert J. Rovetto 《Earth Science Informatics》2017,10(4):417-427
This paper demonstrates the development of ontology for satellite databases. First, I create a computational ontology for the Union of Concerned Scientists (UCS) Satellite Database (UCSSD for short), called the UCS Satellite Ontology (or UCSSO). Second, in developing UCSSO I show that The Space Situational Awareness Ontology (SSAO) (Rovetto & Kelso 2016)-—an existing space domain reference ontology—-and related ontology work by the author (Rovetto 2015, 2016) can be used either (i) with a database-specific local ontology such as UCSSO, or (ii) in its stead. In case (i), local ontologies such as UCSSO can reuse SSAO terms, perform term mappings, or extend it. In case (ii), the author’s orbital space ontology work, such as the SSAO, is usable by the UCSSD and organizations with other space object catalogs, as a reference ontology suite providing a common semantically-rich domain model. The SSAO, UCSSO, and the broader Orbital Space Environment Domain Ontology project is online at https://purl.org/space-ontology and GitHub. This ontology effort aims, in part, to provide accurate formal representations of the domain for various applications. Ontology engineering has the potential to facilitate the sharing and integration of satellite data from federated databases and sensors for safer spaceflight. 相似文献
18.
系统锚杆对三峡船闸高边坡岩体加固作用的块体相似模型试验研究 总被引：22，自引：4，他引：22
通过室内相似模型试验，对三峡船闸高边坡岩体的分离块体经系统锚杆加固后，其抗压强度、弹性模量及Ｃ、值的提高、锚固岩体的各向异性进行了初步研究，得出了相应的结论。 相似文献
19.
Turkey established the TUSAGA-AKTIF CORS Network in May 2009. Network software and central server were updated in 2016. With this update, GLONASS message type was determined for Flächen Korrektur Parameter (FKP), Master Auxiliary Concept (MAC) and Virtual Reference Station (VRS) network-based real time kinematic (NRTK) techniques. A 64 bit central server and the Trimble Pivot Platform network software were also acquired with this update. To the best of our knowledge, there has not been a comprehensive accuracy and precision test of the new system yet. In this paper, we aimed to create empirical accuracy and precision model of FKP, MAC and VRS NRTK techniques of the updated system as a function of baseline distance and occupation time. It is intended that surveyors can perform mission planning according to the requirements of accuracy and precision using these models. Seven test points and two check points were chosen to conduct the experiment. The baseline lengths with respect to the closest continuously operating reference stations (CORS) station were determined as 5-20-40-50 km approximately. Three thousand epochs with 2-s sampling interval were obtained for northing, easting and ellipsoidal height coordinate components of NRTK techniques at each point. Assumed true coordinates of each test point were determined by static survey using the GAMIT/GLOBK scientific software. In terms of accuracy and precision, our results show that empirical accuracy model depends only on the occupation time while empirical precision model depends on both the baseline length with respect to the closest CORS station and the occupation time for each NRTK technique. The results indicate that estimated accuracy and precision models can be safely used for mission planning purposes. 相似文献
20.
针对非饱和重塑黏土,利用改进的非饱和土静力-动力液压三轴-扭转多功能剪切仪,在固结排水（CD）条件下进行了应力控制式分级加载的循环三轴试验,通过对试验结果的对比分析,探讨了初始固结压力和基质吸力(孔隙气压力Ua与孔隙水压力Uw之差)对非饱和土动应力-动应变关系特性的影响。以此为基础,将Hardin-Drnerich等价黏弹性模型和Masing加卸载准则进行了改进,并得到了可以考虑基质吸力的非饱和黏土的等价黏弹性模型。进而对试验数据与模型预测结果进行比较,结果表明这种改进的非饱和土等价黏弹性模型能较好预测各种基质吸力下非饱和土的动应力-动应变关系。 相似文献