• DocumentCode
    2589787
  • Title

    Acceleration “G” compensated quartz crystal oscillators

  • Author

    Bloch, M. ; Mancini, O. ; McClelland, T. ; Terracciano, L.

  • Author_Institution
    Freq. Electron., Inc., Mitchel Field, NY, USA
  • fYear
    2009
  • fDate
    20-24 April 2009
  • Firstpage
    175
  • Lastpage
    180
  • Abstract
    High dynamic environments common to most platforms in motion such as helicopters, track-vehicles, ships, missiles and even spacecraft degrade the performance of quartz crystal oscillators. To generate the precise frequencies and time signals crucial to system performance quartz crystal oscillators and rubidium vapor atomic oscillators are commonly utilized. However quartz crystal oscillators whether stand alone or parts of traditional rubidium oscillators, exhibit degraded performance when subject to accelerating forces, i.e. sine and/or random vibrations. Although the spacecraft environment has traditionally been considered ldquovibration-free,rdquo it is increasingly clear that low level accelerations and vibrations due to reaction wheels, thrusters, etc. degrade quartz oscillator output enough to impact, in many cases, system level performance. In addition, mechanical vibrations in ground stations/gateways degrade quartz oscillator performance and greatly affect beam-forming networks for communications satellites. In this paper we shall discuss a ldquogrdquo (acceleration) compensated technology that has greatly increased the performance of quartz crystal oscillators in challenging environments. We will present data on technology break-through in two main areas (a) new methods of quartz resonator design and manufacturing that result in minimum cross-coupling between the three resonator axes and (b) new sensing devices that can be mounted and aligned in each resonator axis. In addition, we will present actual test data for oscillators performing in high ldquogrdquo environments as well as lower ldquogrdquo environments such as in spacecraft and ground stations/gateways.
  • Keywords
    crystal oscillators; space vehicle electronics; vibrations; beam-forming network; communications satellites; helicopters; high dynamic environment; mechanical vibration; missiles; quartz crystal oscillator; rubidium oscillator; rubidium vapor atomic oscillator; ships; spacecraft environment; track vehicles; Acceleration; Degradation; Helicopters; Marine vehicles; Missiles; Oscillators; Satellite ground stations; Space vehicles; Tracking; Vibrations;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Frequency Control Symposium, 2009 Joint with the 22nd European Frequency and Time forum. IEEE International
  • Conference_Location
    Besancon
  • ISSN
    1075-6787
  • Print_ISBN
    978-1-4244-3511-1
  • Electronic_ISBN
    1075-6787
  • Type

    conf

  • DOI
    10.1109/FREQ.2009.5168164
  • Filename
    5168164