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  • 1
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    American Association for the Advancement of Science (AAAS)
    Publication Date: 2006-05-06
    Description: 〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Marty, Bernard -- New York, N.Y. -- Science. 2006 May 5;312(5774):706-7.〈br /〉〈span class="detail_caption"〉Author address: 〈/span〉Centre de Recherches Petrographiques et Geochimiques, Vandoeuvre-les-Nancy Cedex, 54501 France. bmarty@crpg.cnrs-nancy.fr〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/16675689" target="_blank"〉PubMed〈/a〉
    Keywords: *Cosmic Dust ; Deuterium/*analysis ; Evolution, Planetary ; *Meteoroids ; Nitrogen Isotopes/*analysis ; Organic Chemicals/*analysis ; Oxygen Isotopes ; *Solar System ; Ultraviolet Rays
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 2
    Publication Date: 2012-10-16
    Description: Tissint (Morocco) is the fifth martian meteorite collected after it was witnessed falling to Earth. Our integrated mineralogical, petrological, and geochemical study shows that it is a depleted picritic shergottite similar to EETA79001A. Highly magnesian olivine and abundant glass containing martian atmosphere are present in Tissint. Refractory trace element, sulfur, and fluorine data for the matrix and glass veins in the meteorite indicate the presence of a martian surface component. Thus, the influence of in situ martian weathering can be unambiguously distinguished from terrestrial contamination in this meteorite. Martian weathering features in Tissint are compatible with the results of spacecraft observations of Mars. Tissint has a cosmic-ray exposure age of 0.7 +/- 0.3 million years, consistent with those of many other shergottites, notably EETA79001, suggesting that they were ejected from Mars during the same event.〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Aoudjehane, H Chennaoui -- Avice, G -- Barrat, J-A -- Boudouma, O -- Chen, G -- Duke, M J M -- Franchi, I A -- Gattacceca, J -- Grady, M M -- Greenwood, R C -- Herd, C D K -- Hewins, R -- Jambon, A -- Marty, B -- Rochette, P -- Smith, C L -- Sautter, V -- Verchovsky, A -- Weber, P -- Zanda, B -- New York, N.Y. -- Science. 2012 Nov 9;338(6108):785-8. doi: 10.1126/science.1224514. Epub 2012 Oct 11.〈br /〉〈span class="detail_caption"〉Author address: 〈/span〉Hassan II University Casablanca, Faculty of Sciences, Geosciences Appliquees a l'Ingenierie et l'Amenagement (GAIA) Laboratory, BP 5366 Maarif, Casablanca, Morocco. chennaoui_h@yahoo.fr〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/23065902" target="_blank"〉PubMed〈/a〉
    Keywords: Carbon Isotopes/analysis ; Iron Compounds/analysis ; Magnesium Compounds/analysis ; *Mars ; *Meteoroids ; Nitrogen Isotopes/analysis ; Oxygen Isotopes/analysis ; Silicates/analysis
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 3
    Publication Date: 2006-12-16
    Description: Hydrogen, carbon, nitrogen, and oxygen isotopic compositions are heterogeneous among comet 81P/Wild 2 particle fragments; however, extreme isotopic anomalies are rare, indicating that the comet is not a pristine aggregate of presolar materials. Nonterrestrial nitrogen and neon isotope ratios suggest that indigenous organic matter and highly volatile materials were successfully collected. Except for a single (17)O-enriched circumstellar stardust grain, silicate and oxide minerals have oxygen isotopic compositions consistent with solar system origin. One refractory grain is (16)O-enriched, like refractory inclusions in meteorites, suggesting that Wild 2 contains material formed at high temperature in the inner solar system and transported to the Kuiper belt before comet accretion.〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉McKeegan, Kevin D -- Aleon, Jerome -- Bradley, John -- Brownlee, Donald -- Busemann, Henner -- Butterworth, Anna -- Chaussidon, Marc -- Fallon, Stewart -- Floss, Christine -- Gilmour, Jamie -- Gounelle, Matthieu -- Graham, Giles -- Guan, Yunbin -- Heck, Philipp R -- Hoppe, Peter -- Hutcheon, Ian D -- Huth, Joachim -- Ishii, Hope -- Ito, Motoo -- Jacobsen, Stein B -- Kearsley, Anton -- Leshin, Laurie A -- Liu, Ming-Chang -- Lyon, Ian -- Marhas, Kuljeet -- Marty, Bernard -- Matrajt, Graciela -- Meibom, Anders -- Messenger, Scott -- Mostefaoui, Smail -- Mukhopadhyay, Sujoy -- Nakamura-Messenger, Keiko -- Nittler, Larry -- Palma, Russ -- Pepin, Robert O -- Papanastassiou, Dimitri A -- Robert, Francois -- Schlutter, Dennis -- Snead, Christopher J -- Stadermann, Frank J -- Stroud, Rhonda -- Tsou, Peter -- Westphal, Andrew -- Young, Edward D -- Ziegler, Karen -- Zimmermann, Laurent -- Zinner, Ernst -- New York, N.Y. -- Science. 2006 Dec 15;314(5806):1724-8.〈br /〉〈span class="detail_caption"〉Author address: 〈/span〉Department of Earth and Space Sciences, University of California Los Angeles, Los Angeles, CA 90095-1567, USA. mckeegan@ess.ucla.edu〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/17170292" target="_blank"〉PubMed〈/a〉
    Keywords: Carbon Isotopes/*analysis ; Deuterium/*analysis ; Hydrogen/analysis ; Isotopes/*analysis ; *Meteoroids ; Neon/analysis ; Nitrogen Isotopes/*analysis ; Noble Gases/analysis ; Oxygen Isotopes/*analysis ; Spacecraft
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 4
    Publication Date: 2016-06-07
    Description: Wavelets present a method for signal processing that may be useful for analyzing responses of dynamical systems. This paper describes several wavelet-based tools that have been developed to improve the efficiency of flight flutter testing. One of the tools uses correlation filtering to identify properties of several modes throughout a flight test for envelope expansion. Another tool uses features in time-frequency representations of responses to characterize nonlinearities in the system dynamics. A third tool uses modulus and phase information from a wavelet transform to estimate modal parameters that can be used to update a linear model and reduce conservatism in robust stability margins.
    Keywords: Aircraft Stability and Control
    Type: CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics 1999; Pt. 1; 393-402; NASA/CP-1999-209136/PT1
    Format: application/pdf
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  • 5
    Publication Date: 2019-07-13
    Description: An approach for computing worst-case flutter margins has been formulated in a robust stability framework. Uncertainty operators are included with a linear model to describe modeling errors and flight variations. The structured singular value, micron, computes a stability margin which directly accounts for these uncertainties. This approach introduces a new method of computing flutter margins and an associated new parameter for describing these margins. The micron margins are robust margins which indicate worst-case stability estimates with respect to the defined uncertainty. Worst-case flutter margins are computed for the F/A-18 SRA using uncertainty sets generated by flight data analysis. The robust margins demonstrate flight conditions for flutter may lie closer to the flight envelope than previously estimated by p-k analysis.
    Keywords: Aircraft Stability and Control
    Type: NASA/TM-97-207564 , NAS 1.15:207564 , AIAA Paper 97-1266 , Structures, Structural Dynamics and Materials Conference; Apr 01, 1997; Orlando, FL; United States
    Format: application/pdf
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  • 6
    Publication Date: 2019-07-13
    Description: Wavelet analysis for filtering and system identification was used to improve the estimation of aeroservoelastic stability margins. The conservatism of the robust stability margins was reduced with parametric and nonparametric time-frequency analysis of flight data in the model validation process. Nonparametric wavelet processing of data was used to reduce the effects of external desirableness and unmodeled dynamics. Parametric estimates of modal stability were also extracted using the wavelet transform. Computation of robust stability margins for stability boundary prediction depends on uncertainty descriptions derived from the data for model validation. F-18 high Alpha Research Vehicle aeroservoelastic flight test data demonstrated improved robust stability prediction by extension of the stability boundary beyond the flight regime.
    Keywords: Aircraft Stability and Control
    Type: NASA/TM-1998-206545 , NAS 1.15:206545 , H-2222 , AIAA Paper 98-1896 , Structures, Structural Dynamics and Materials Conference; Apr 20, 1998 - Apr 23, 1998; Long Beach, CA; United States
    Format: application/pdf
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  • 7
    Publication Date: 2019-07-13
    Description: Modal stability parameters are extracted directly from aeroservoelastic flight test data by decomposition of accelerometer response signals into time-frequency atoms. Logarithmic sweeps and sinusoidal pulses are used to generate DAST closed loop excitation data. Novel wavelets constructed to extract modal damping and frequency explicitly from the data are introduced. The so-called Haley and Laplace wavelets are used to track time-varying modal damping and frequency in a matching pursuit algorithm. Estimation of the trend to aeroservoelastic instability is demonstrated successfully from analysis of the DAST data.
    Keywords: Aircraft Stability and Control
    Type: NASA/TM-97-206300 , NAS 1.15:206300 , H-2214 , Atmospheric Flight Mechanics Conference; Aug 08, 1997 - Aug 11, 1997; New Orleans, LA; United States
    Format: application/pdf
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  • 8
    Publication Date: 2019-07-13
    Description: Stability analysis of high performance aircraft must account for errors in the system model. A method for computing flutter margins that incorporates flight data has been developed using robust stability theory. This paper considers applying this method to update flutter margins during a post-flight or on-line analysis. Areas of modeling uncertainty that arise when using flight data with this method are investigated. The amount of conservatism in the resulting flutter margins depends on the flight data sets used to update the model. Post-flight updates of flutter margins for an F/A-18 are presented along with a simulation of on-line updates during a flight test.
    Keywords: Aircraft Stability and Control
    Type: Atmospheric Flight Mechanics Conference; Aug 01, 1997; New Orleans, LA; United States
    Format: text
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  • 9
    Publication Date: 2019-07-13
    Description: Wavelets present a method for signal processing that may be useful for analyzing responses of dynamical systems. This paper describes several wavelet-based tools that have been developed to improve the efficiency of flight flutter testing. One of the tools uses correlation filtering to identify properties of several modes throughout a flight test for envelope expansion. Another tool uses features in time-frequency representations of responses to characterize nonlinearities in the system dynamics. A third tool uses modulus and phase information from a wavelet transform to estimate modal parameters that can be used to update a linear model and reduce conservatism in robust stability margins.
    Keywords: Aircraft Stability and Control
    Type: H-2364 , International Forum on Aeroelasticity and Structural Dynamics; Jun 22, 1999 - Jun 25, 1999; Williamsburg, VA; United States
    Format: application/pdf
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