DocumentCode :
3597830
Title :
Vibration isolation for autonomous helicopter flight
Author :
Dunbabin, Matthew ; Brosnan, Stephen ; Roberts, Jonathan ; Corke, Peter
Author_Institution :
CSIRO Manuf. & Infrastruct. Technol., Kenmore, NSW, Australia
Volume :
4
fYear :
2004
Firstpage :
3609
Abstract :
The mechanisms of helicopter flight create a unique, high-vibration environment which can play havoc with the accurate operation of on-board sensors. Vibration isolation of electronic sensors from structural borne oscillations is paramount to their reliable and accurate use. Effective isolation is achieved by realising a trade-off between the properties of the suspended instrument package, and the isolation mechanism. This is made more difficult as the weight and size of the sensors and computing hardware decreases with advances in technology. This paper presents a history of the design, challenges, constraints and construction of an integrated isolated vision and sensor platform and landing gear for the CSIRO autonomous X-Cell helicopter. The results of isolation performance and in-flight tests of the platform in autonomous flight are presented.
Keywords :
aerospace robotics; aircraft testing; avionics; helicopters; mobile robots; sensors; vibration isolation; CSIRO autonomous X-Cell helicopter; autonomous helicopter flight; electronic sensors; hardware computing; in-flight tests; integrated isolated vision; isolation mechanism; landing gear; onboard sensors; sensor platform; structural borne oscillations; suspended instrument package; vibration isolation; Aerospace electronics; Electronics packaging; Gears; Hardware; Helicopters; History; Instruments; Isolation technology; Mechanical factors; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Robotics and Automation, 2004. Proceedings. ICRA '04. 2004 IEEE International Conference on
ISSN :
1050-4729
Print_ISBN :
0-7803-8232-3
Type :
conf
DOI :
10.1109/ROBOT.2004.1308812
Filename :
1308812
Link To Document :
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