Measuring Moment of Inertia of RC Helicopter

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SUMMARY

This discussion focuses on measuring the moment of inertia of a remote-controlled helicopter about its three principal axes at the center of gravity. The user outlines equations relating angular accelerations to moments and moments of inertia, specifically p_dot, q_dot, and r_dot equations. An experimental setup involving rotating the helicopter on a table is proposed, although challenges regarding torque measurement are acknowledged. The user also mentions the use of gyros and accelerometers for accurate measurements and references additional resources from Space Electronics for further guidance.

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  • Understanding of angular motion and inertia principles
  • Familiarity with gyroscopic and accelerometer measurement techniques
  • Knowledge of rotational dynamics equations
  • Experience with experimental physics setups
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williamshipman
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Hi guys.

I am trying to measure the moment of inertia of a remote controlled helicopter about its 3 principle axes at the centre of gravity. In all of the literature I have read relating to this project, everyone just glosses over this part. What I need to figure out is an experimental setup and method.

I have the following 3 equations that relate the moment about each axis and the 3 angular velocities to the angular accelerations. All of these equations are with respect a fixed axis system centred at the centre of gravity.
p_dot=M_x/I_xx -rq/I_xx (I_zz-I_yy )
q_dot=M_y/I_yy -rp/I_yy (I_xx-I_zz )
r_dot=M_z/I_zz -pq/I_zz (I_yy-I_xx )

p_dot, q_dot and r_dot are the angular accelerations. The angular velocities are p (roll), q (pitch) and r (yaw). The moments about each axis are M_x, M_y and M_z and the moments of inertia are I_xx, I_yy and I_zz.

So far, I have thought of putting the helicopter on a table and rotating it about one axis, then repeating the procedure for the other 2 axes. This has the small problem that, if the table rotates at a constant rate, the dot terms are zero. If the table is accelerating, then this could work but how would I know what the torque applied to the helicopter is?

I forgot to mention, the helicopter will be fitted with gyros to measure the orientation and accelerometers for the linear and angular accelerations. Thanks for your help.
 
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It's not the easiest way to do things, but it is definitely doable. I guess it all boils down to how accurate you want to get. You can measure the principal axes via the method in the attached article. The off diagonal elements you can then calculate.

Go to this thread for the article:
https://www.physicsforums.com/showthread.php?t=222753
 


Thanks very much for the info Fred, that was exactly what I was looking for.
 


Its now a few months later and I thought I'd post this. FredGarvin gave a paper from Space Electronics in the other thread he links to. Space Electronics has published a number of other papers on their website that explain how to measure various properties, like the moment of inertia and center of gravity. Anyone who is struggling with such work should look at their website http://www.space-electronics.com" .
 
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