This paper describes the avionics developed for a miniature acrobatic helicopter and the applications for such a system. The avionics system is designed to safely achieve a robust, high-bandwidth feedback control system while meeting physical specifications. The system that is currently implemented has provided an efficient platform for testing new closed-loop controllers and has yielded critical flight data used for developing simple models of small-scale helicopter dynamics. The helicopter has already demonstrated successful flight under a body-axis velocity/heading rate-tracking controller.
Design and applications of an avionics system for a miniature acrobatic helicopter
20th DASC. 20th Digital Avionics Systems Conference (Cat. No.01CH37219) ; 1 ; 3C5/1-3C5/10 vol.1
2001-01-01
926985 byte
Conference paper
Electronic Resource
English
Design and Applications of an Avionics System for a Miniature Acrobatic Helicopter
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