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Measuring Mass Moment of Inertia with a Bifilar Pendulum

version 1.5.0.1 (2.9 MB) by Matt Jardin
A Simulink® model of a bifilar pendulum for measuring mass moment of inertia.

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Updated 01 Sep 2016

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The bifilar pendulum is a torsional pendulum that can be used to experimentally measure the mass moment of inertia of a test object. A typical application is to measure mass moment of inertia of aircraft, especially small unmanned air vehicles (UAV). This model corresponds to the one discussed in the following article:
Jardin, M., Mueller, E., "Optimized Measurements of Unmanned Air Vehicle Mass Moment of Inertia with a Bifilar Pendulum," Journal of Aircraft, Vol. 46, No. 3, May-June 2009, pp. 763-775.
This paper was also presented at the AIAA GNC Conference in 2007:
Jardin, M., Mueller, E., "Optimized Measurements of UAV Mass Moment of Inertia with a Bifilar Pendulum," AIAA-2007-6822, AIAA GNC Conference, Hilton Head, SC, Aug. 20-23, 2007.

Comments and Ratings (1)

Arizal Akbar Zikri

Updates

1.5.0.1

Updated license

1.5.0.0

Added copyright statement to BP_exampleParams.m

1.4.0.0

Updated reference to more recent journal article.

1.2.0.0

Model has been updated for Release R2009a. Simulink Parameter Estimation tasks have been included.

1.0.0.0

Added the words "parameter estimation" to the keywords list so that anyone looking for examples using Simulink Parameter Estimation will find this submission.

Updated AIAA paper number in the Description.

MATLAB Release Compatibility
Created with R2009a
Compatible with any release
Platform Compatibility
Windows macOS Linux

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