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