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Simulation and flight test of a temperature sensing stabilisation system

Published online by Cambridge University Press:  03 February 2016

P. Herrmann  and
C. Bil
P. Herrmann
Affiliation:
Sir Lawrence Wackett Centre for Aerospace Design Technology, School of Aerospace, Mechanical and Manufacturing Engineering, RMIT University, Melbourne, Australia
C. Bil
Affiliation:
Sir Lawrence Wackett Centre for Aerospace Design Technology, School of Aerospace, Mechanical and Manufacturing Engineering, RMIT University, Melbourne, Australia
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Abstract

Thermopile sensors detect electromagnetic radiation as a function of the object’s temperature. Because there is a temperature difference between the cold ground and the warm sky, these sensors could be used to detect the horizon and thus be used as a reference to stabilise a small aircraft, such as an unmanned aerial vehicle (UAV) in visual meteorological conditions (VMC). To verify this hypothesis, a system has been developed providing horizon detection using thermopile sensors to stabilise an R/C model aircraft. The aircraft has gone through a number of flight trials using remote control to enable and disable the stabilisation system. During the flight trials the aircraft was set at various attitudes when the system was enabled. The stabilisation system was able to assume wing level under various bank angles and weather conditions with minimum overshoot and oscillation.

Although the system shows good performance during flight trials, most of the original design was done using trial and error. A design tool was needed to implement further improvements to the system and to efficiently implement it on other aircraft. This required a good understanding of the physical behaviour of the system and the interaction between the sensors, aircraft and the environment. A mathematical model of the overall system was developed using the MATLAB/Simulink environment to simulate the behaviour of the system under various conditions. The simulation results were then compared with actual flight experiments. This paper describes the modelling techniques used for the different system components and the results of the simulation compared to actual flight trials.

Type
Research Article
Information
The Aeronautical Journal , Volume 109 , Issue 1094 , April 2005 , pp. 167 - 175
Copyright
Copyright © Royal Aeronautical Society 2005 

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