department of geomatics
 
Modelling the PC9 Trainer

PC-9 Deformation Analysis - DSTO

Photogrammetry was used used to perform a complex deformation measurement of an entire PC-9 Aircraft. The work formed part of a 'Fatigue Test Simulator' that simulates real flight scenarios. The array of actuators connected to the aircraft simulate real flying conditions on the airframe. This process allows DSTO to safely take the aircraft to, and beyond, its operational limits. The airframe is routinely stripped down and assessed for damage such as fatigue and cracking. This allows DSTO to isolate and combat problems in the PC-9 well before they occur in the aircraft.

The measurement goal was to accurately quantify the movement occurring in the airframe for a series of flight loadings. The airframe was measured in 8 different states ranging from zero load to maximum g loading using the V-STARS S-System

For each state, a complex network of 100 images determined the XYZ coordinates of 280 points to better then 0.15mm.

The measurement data was used to refine DSTO's simulation models. Particular interest was paid to the amount of twist occurring in the fuselage under a high g roll manoeuvre. As the airframe ages the amount of fuselage twist increases.



The diagram above is an overlay of the PC9 in a zero-g loading position verses a high g loading. The white and green dots are the locations of the retro-reflective targets. The red lines are 'exaggerated' differences, or point displacement, between the two data sets. The magnitude and direction of the red lines represent displacement vectors between the zero loading and the high g loading.


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Created: 20 April 2004
Last modified: 16th Octoverl 2004
Vision Metrology Services
Email: danny@metrology.com.au