@inproceedings{0437b9a780444217a889bb8c184de298,
title = "Silicon micromechanical tuning output gyroscope applied at navigation of micro unmanned aerial vehicle",
abstract = "Silicon micromechanical tuning output gyroscope utilizes resonant sensing as the basis for Coriolis force detection instead of displacement sensing. The text gives out the dynamics equation of system and puts forward a kind of new structure form which avoids the influence of non-ideal electrostatic and mechanical cross-coupling. Based on the mechanical vibration principle, the response of a resonant system to an external static and dynamic axial load has been analyzed in the text Simulation results display that it can provide effective gesture information For the micro unmanned aerial vehicle.",
author = "Jianli Li and Jiancheng Fang and Wenbo Yu",
year = "2005",
language = "英语",
isbn = "1563477378",
series = "Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference",
pages = "6474",
booktitle = "Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2005",
note = "AIAA Guidance, Navigation, and Control Conference 2005 ; Conference date: 15-08-2005 Through 18-08-2005",
}