REAL-TIME COMPUTATIONS OF PILOT BALLOON WINDS

Abstract

The report shows that the mean wind through a given altitude layer can be determined from balloon tracking data without computing wind values for individual points within the altitude layer. The assumptions involved in the procedure are similar to the assumption made in numerical differentiating techniques, i.e., the position can be approximated by a polynomial. Two such techniques are investigated. One uses a linear equation to approximate the position; the other uses a cubic equation. These techniques were applied to balloon data from 27 balloon tracks and compared with results obtained from numerical differentiation. It is shown that there is very little difference among the results of the various calculation procedures.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1968
Accession Number
AD0667923

Entities

People

  • Bernard F. Engebos
  • Louis D. Duncan

Organizations

  • Atmospheric Sciences Laboratory

Tags

Communities of Interest

  • Sensors
  • Weapons Technologies

DTIC Thesaurus Topics

  • Acoustic Propagation
  • Acoustic Waves
  • Altitude
  • Atmospheric Motion
  • Atmospheric Sciences
  • Computations
  • Electromagnetic Scattering
  • Equations
  • High Altitude
  • Measurement
  • New Mexico
  • Pressure Measurement
  • Sound Ranging
  • Trajectories
  • Turbulence
  • Wind
  • Wind Velocity

Readers

  • Computational Modeling and Simulation
  • Fault Tolerant Diagnosis of Black and White Balloon Isolation Tests Using ¥.
  • Operations Research