Książki na temat „Accelerometer”

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1

Dauderstädt, Ulrike Anna. A thermal accelerometer. Delft: Delft University Press, 1999.

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2

Olcott, Joanne E. Fiber-optic flexural disk accelerometer. Monterey, Calif: Naval Postgraduate School, 1991.

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3

B, Rogers Melissa J., i United States. National Aeronautics and Space Administration., red. Accelerometer data analysis and presentation techniques. [Washington, D.C: National Aeronautics and Space Administration, 1997.

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4

John, Lekki, i NASA Glenn Research Center, red. A self-diagnostic system for the M6 accelerometer. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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5

John, Lekki, i NASA Glenn Research Center, red. A self-diagnostic system for the M6 accelerometer. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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6

B, Rogers Melissa J., i United States. National Aeronautics and Space Administration., red. USML-1 microgravity glovebox experiment 1 passive accelerometer system. [Washington, DC: National Aeronautics and Space Administration, 1995.

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7

B, Rogers Melissa J., i United States. National Aeronautics and Space Administration., red. USML-1 microgravity glovebox experiment 1 passive accelerometer system. [Washington, DC: National Aeronautics and Space Administration, 1995.

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8

B, Rogers Melissa J., i United States. National Aeronautics and Space Administration., red. USML-1 microgravity glovebox experiment 1 passive accelerometer system. [Washington, DC: National Aeronautics and Space Administration, 1995.

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9

DeLombard, Richard. Proposed ground-based control of accelerometer on Space Station Freedom. [Washington, DC: National Aeronautics and Space Administration, 1993.

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10

DeLombard, Richard. Proposed ground-based control of accelerometer on Space Station Freedom. [Washington, DC: National Aeronautics and Space Administration, 1993.

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11

DeLombard, Richard. Proposed ground-based control of accelerometer on Space Station Freedom. [Washington, DC: National Aeronautics and Space Administration, 1993.

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12

Chipkevich, Mary Beth A. Design and fabrication of a fiber-optic interferometric accelerometer system. Monterey, Calif: Naval Postgraduate School, 1992.

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13

United States. National Aeronautics and Space Administration., red. Proposed ground-based control of accelerometer on Space Station Freedom. [Washington, DC: National Aeronautics and Space Administration, 1993.

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14

United States. National Aeronautics and Space Administration., red. Accelerometer placement for the International Space Station Node modal test. [Washington, D.C: National Aeronautics and Space Administration, 1998.

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15

Boyce, Christine. Comparison of energy expenditure using the CSA accelerometer and two questionnaires. [s.l: The Author], 1997.

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16

United States. National Aeronautics and Space Administration., red. Modelling of the MEA float zone using accelerometer data: Final report. Huntsville, Ala: Center for Microgravity and Materials and Materials Research, The University of Alabama in Huntsville, 1993.

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17

C, Shaw Harry, i Goddard Space Flight Center, red. Dynamic response assessment for the MEMS accelerometer under severe shock loads. Greenbelt, Md: National Aeronautics and Space Administration, Goddard Space Flight Center, 2001.

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18

H, Canton, red. The comparison of European laboratories dealing with middle frequency accelerometer calibration. Luxembourg: Commission of the European Communities, 1986.

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19

R, Evans John. The design and performance of a low-cost strong-motion sensor using the ICS-3028 micromachined accelerometer. [Reston, Va.?]: U.S. Dept. of the Interior, U.S. Geological Survey, 1998.

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20

R, Evans John. The design and performance of a low-cost strong-motion sensor using the ICS-3028 micromachined accelerometer. [Reston, Va.?]: U.S. Dept. of the Interior, U.S. Geological Survey, 1998.

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21

Geological Survey (U.S.), red. The design and performance of a low-cost strong-motion sensor using the ICS-3028 micromachined accelerometer. [Reston, Va.?]: U.S. Dept. of the Interior, U.S. Geological Survey, 1998.

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22

Blanchard, Robert C. The high resolution accelerometer package (HiRAP) flight experiment summary for the first 10 flights. [Washington D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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23

Collins, Emmanuel G. High performance, accelerometer-based control of the Mini-MAST structure at Langley Research Center. Hampton, Va: Langley Research Center, 1991.

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24

E, Collins, Harris Corporation. Government Aerospace Systems Division., Langley Research Center i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. High performance, accelerometer-based control of the mini-MAST structure at Langley Research Center. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

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25

Blanchard, Robert C. The High Resolution Accelerometer Package (HiRAP) flight experiment summary for the first 10 flights. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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26

Blanchard, Robert C. The high resolution accelerometer package (HiRAP) flight experiment summary for the first 10 flights. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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27

Blanchard, Robert C. Ground and flight calibration assessment of HiRAP accelerometer data from missions STS-35 and STS-40. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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28

Blanchard, Robert C. Ground and flight calibration assessment of HiRAP accelerometer data from missions STS-35 and STS-40. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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29

H, Tolson Robert, Keating Gerald M i Langley Research Center, red. Operational data reduction procedure for determining density and vertical structure of the Martian upper atmosphere from Mars global surveyor accelerometer measurements. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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30

Levinzon, Felix. Piezoelectric Accelerometers with Integral Electronics. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-08078-9.

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31

Varum, Humberto, i Sérgio de Brito André. Accelerometers: Principles, structure and applications. Hauppauge, New York: Nova Science Publishers, Inc., 2011.

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32

A, Rogers John, i Geological Survey (U.S.), red. Relative performance of several inexpensive accelerometers. [Reston, Va.]: U.S. Dept. of the Interior, U.S. Geological Survey, 1995.

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33

C, Blanchard Robert, Larman K. T i Langley Research Center, red. Improved HIRAP flight calibration technique. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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34

Xu, Yong Ping. MEMS Silicon Oscillating Accelerometers and Readout Circuits. New York: River Publishers, 2022. http://dx.doi.org/10.1201/9781003338826.

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35

Micro mechanical transducers: Pressure sensors, accelerometers, and gyroscopes. New York: Elsevier Science B.V., 2000.

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36

Andreĭchenko, K. P. Dinamika poplavkovykh giroskopov i akselerometrov. Moskva: "Mashinostroenie", 1987.

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37

H, Morgan Samuel, Paik Ho Jung i George C. Marshall Space Flight Center., red. Superconducting gravity gradiometer mission. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1989.

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38

Moseley, V. J. "Jon", Andreas Lampropoulos, Eftychia Apostolidi i Christos Giarlelis. Characteristic Seismic Failures of Buildings. Redaktor Stephanos E. Dritsos. Zurich, Switzerland: International Association for Bridge and Structural Engineering (IABSE), 2019. http://dx.doi.org/10.2749/sed016.

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Streszczenie:
<p>Earthquakes can cause considerable fatalities, injuries and financial loss. The forces of nature cannot be blamed, as the problem lies with the structures in seismic regions that may not have been designed or constructed to a sufficient degree to resist earthquake actions or they may have design flaws. This Structural Engineering Document (SED) concerns reinforced concrete and masonry buildings together with geotechnical aspects and presents in a concise and practical way the state of the art of current understanding of building failures due to earthquakes. It classifies the different types of seismic failure, explains the reasons for each failure, describes good practices to avoid such failures and also describes seismic retrofitting/upgrading procedures for pre-earthquake strengthening and post-earthquake repair and/or strengthening techniques for deficient buildings. Carefully selected photographs and diagrams illustrate the different failure types. This document could be considered as quite unique, as this is the first time such material concerning characteristic seismic failures of buildings has been presented together in one single document. It is intended to be a valuable educational reference textbook aimed at all levels of experience of engineers. It provides background information, ideas, guidance and reassurance to engineers in earthquake regions faced with the task of building a safer future for the public and to protect lives. <p> <iframe width="560" height="315" src="https://www.youtube-nocookie.com/embed/Oddi3VTtxCM" frameborder="0" allow="accelerometer; autoplay; encrypted-media; gyroscope; picture-in-picture" allowfullscreen></iframe>
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39

H, Morgan Samuel, Paik Ho Jung i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. Superconducting gravity gradiometer mission. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1988.

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40

IEEE Aerospace and Electronic Systems Society. Gyro and Accelerometer Panel., IEEE-SA Standards Board, American National Standards Institute i Institute of Electrical and Electronics Engineers., red. IEEE recommended practice for precision centrifuge testing of linear accelerometers. New York, NY: Institute of Electrical and Electronics Engineers, 2001.

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41

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. Recovery of pyroshock data from distorted acceleration records. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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42

Thomas, John E. Space acceleration measurement system triaxial sensor head error budget. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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43

R, Peřestý, red. Project CESAR: (papers relevant to microaccelerometric experiment MACEK). [Prague?: Astronomical Institute of the Academy of Sciences of the Czech Republic], 1994.

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44

Y, Nicholson John, Ritter J. R i Langley Research Center, red. STS-40 orbital acceleration research experiment flight results during a typical sleep period. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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45

Blanchard, Robert C. STS-40 orbital acceleration research experiment flight results during a typical sleep period. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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46

Jer-Nan, Juang, i Langley Research Center, red. Experimental robot position sensor fault tolerance using accelerometers and joint torque sensors. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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47

Dunbar, Bonnie J. The microgravity environment of the Space Shuttle Columbia payload bay during STS-32. Houston, Tex: Lyndon B. Johnson Space Center, 1991.

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48

Robinson, D. C. Requirements for the calibration of mechanical shock transducers. Gaithersburg, MD: U.S. Dept. of Commerce, National Bureau of Standards, 1987.

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49

Robinson, D. C. A description of NBS calibration services in mechanical vibration and shock. Gaithersburg, MD: U.S. Dept. of Commerce, National Bureau of Standards, 1987.

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50

Practical MEMS. [Las Vegas, Nev.]: Small Gear Pub., 2009.

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