Circuits, Communications and Systems, Pacific-Asia Conference on (2009)
May 16, 2009 to May 17, 2009
By reasonably predigesting the characteristics of the subminiature rotorcraft, a model for a subminiature rotorcraft is established and the linear time-invariant attitude dynamics with physical parameter of the subminiature rotorcraft at hover is obtained. A subspace-based state space system identification method and analysis of model uncertainty is applied to the model of rotorcraft. At last, the valid of the identified attitude model is testified.
subminiature rotorcraft, mathematical modeling, system identification
Zhengbang Gong, Tongyue Gao, Wei Feng, Jun Luo, "Mathematical Modeling and Identification of a Subminiature Rotorcraft with Flybar Dynamics", Circuits, Communications and Systems, Pacific-Asia Conference on, vol. 00, no. , pp. 364-367, 2009, doi:10.1109/PACCS.2009.168