A Microprocessor-Based Data-Acquisition System for Stall/Spin Research

M. Sri-Jayantha, Robert Frank Stengel

Research output: Contribution to journalArticle

4 Scopus citations

Abstract

Accurate data are necessary for the identification of aerodynamic parameters at high angle of attack and in spinning flight. Modern sensors and microelectronic devices are employed in a stall/ spin data acquisition system that will be tested in a Schweizer 2-32 sailplane. This instrumentation package will use a quaternion-based “strapdown IMU” algorithm to derive vehicle attitude from angular rate data, and it will use fault-detection logic to identify inflight sensor failures. Details of the system and flight test program are presented, together with results of preflight digital simulation analysis.

Original languageEnglish (US)
Pages (from-to)59-70
Number of pages12
JournalIEEE Transactions on Aerospace and Electronic Systems
VolumeAES-19
Issue number1
DOIs
StatePublished - Jan 1 1983

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Electrical and Electronic Engineering

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