Attitude Model Identification for Sub-Mini Dual Ducted UAV under Hovering
Attitude Model Identification for Sub-Mini Dual Ducted UAV under Hovering
- New search for: Gao, Tong Yue
- New search for: Wang, Dong Dong
- New search for: Tao, Fei
- New search for: Ge, Hai Lang
Based on the sub-mini dual ducted UAV dynamics analysis of Newton, and according to the characteristics of the hovering and variable posture mechanism, this paper combined methods of mechanism analysis with system identification to get the attitude model of under actuated sub-mini dual ducted UAV, which contained input variable, output variable and some unknown parameters. Then the subspace method used the real flying data to identify above the attitude model. Finally，the correctness of the identification model was verified.
Document information
Attitude Model Identification for Sub-Mini Dual Ducted UAV under Hovering
Applied Mechanics and Materials ; 513-517 ; 2812-2815
2014-02-06
4 pages
Article (Journal)
Electronic Resource
English
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