1887
Volume 37, Issue 4
  • ISSN: 0812-3985
  • E-ISSN: 1834-7533

Abstract

Helicopter electromagnetic systems typically have a transmitter-receiver coil pair in a towed bird that, in flight, behaves as a complex compound pendulum. Pendulum motions of the towed bird create not only a geometric and inductive effect in the measured signal, but they may also contribute to altitude error. The oscillation of the towed-bird pendulum can be observed from both video recordings and GPS positions and is most usefully broken down into two modes: one in the direction of travel (in-line) and one perpendicular to the direction of travel (cross-line). We analyse the electromagnetic and altitude data for a RESOLVE survey on the Chowilla flood plain, near Renmark, South Australia. The in-line and cross-line motions of the towed bird are shown to have different frequencies of oscillation. In-line motions, which cause pitching of the towed bird, and cross-line motions, which generate roll, create a systematic error in data easily evident in the dimensionless in-phase divided by inductive limit domain. We show that the bird swing due to both modes of pendulum motion is responsible for altitude error, and that a filter designed to use the observed period of oscillation can largely correct the domain data. The filtering process does not require any more measurements than are usually provided from a typical electromagnetic survey.

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/content/journals/10.1071/EG06355
2006-12-01
2026-01-17
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References

  1. Fitterman, D.V., and Yin, C, 2004, Effect of bird maneuver on frequency-domain helicopter EM response: Geophysics , 69, 1203-1215.
  2. Fowles, G.R., and Cassiday, G.L., 1993, Analytical Mechanics: Saunders College Publishing.
  3. Holladay, J.S., Lo, B., and Prinsenberg, S.K., 1997, Bird orientation effects in quantitative airborne electromagnetic interpretation of pack ice thickness sounding: Oceans ’97 , MTS (Marine Technology Society)/IEEE, 1114-1116.
  4. Kratzer, T., and Vrbancich, J., 2006, Real-time kinematic tracking of towed AEM birds: Exploration Geophysics , 38, (in press).
  5. Ley-Cooper, Y., Macnae, J., Robb, T., and Vrbancich, J., 2006, Identification of calibration errors in helicopter electromagnetic (HEM) data through transform to the altitude-corrected phase-amplitude domain: Geophysics , 71, G27-G34.
  6. Yin, C, and Fraser, D.C., 2004, Attitude corrections of helicopter EM data using a superposed dipole model: Geophysics , 69, 431-439.
/content/journals/10.1071/EG06355
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  • Article Type: Research Article
Keyword(s): altimeter error; attitude; bird swing; HEM; manoeuvre; pendulum motion

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