Attitude Model Identification for Sub-Mini Dual Ducted UAV under Hovering
2014 ◽
Vol 513-517
◽
pp. 2812-2815
Keyword(s):
The Real
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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.
2021 ◽
Vol 3
(1)
◽
pp. 13-19
2021 ◽
Vol 1887
(1)
◽
pp. 012017
2008 ◽
Vol 2008
(0)
◽
pp. _526-1_-_526-6_
1991 ◽
Vol 38
(9)
◽
pp. 1030-1042
◽
Keyword(s):
Keyword(s):
2022 ◽