Flatus
发表于 2025-3-25 05:33:38
https://doi.org/10.1007/978-3-322-87682-9es. In this paper, in order to reduce the effect of noise covariance uncertainty, the Fuzzy Adaptive Iterated Extended Kalman Filter (FAIEKF) and Fuzzy Adaptive Unscented Kalman Filter (FAUKF) are proposed to overcome this drawback. The proposed FAIEKF and FAUKF have been applied to fuse signals fro
羽饰
发表于 2025-3-25 11:14:40
https://doi.org/10.1007/978-1-4039-8454-8ty analysis, . reveals how the solution of the optimization problem (worst case) changes when we perturb the parameters under consideration. The method is illustrated by testing a vertical take-off and landing vehicle with an . controller for height loss during the transition phase.
callous
发表于 2025-3-25 13:47:59
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prick-test
发表于 2025-3-25 19:52:29
Flight Control Law Testing Using Optimal Control and Postoptimal Sensitivity Analysis978-3-658-31279-4
Antigen
发表于 2025-3-25 21:47:35
Limit Cycle Oscillation Amplitude Tailorng Based on Describing Functions and , Analysis978-3-658-09251-1
Banister
发表于 2025-3-26 03:07:42
Development of an Automatic Flight Path Controller for a DA42 General Aviation Aircraft978-3-662-25048-8
Atheroma
发表于 2025-3-26 04:47:18
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跳动
发表于 2025-3-26 09:54:14
Identification of a Cessna Citation II Model Based on Flight Test Data978-3-322-83987-9
Resign
发表于 2025-3-26 14:38:43
Advances in Aerospace Guidance, Navigation and ControlSelected Papers of t
混合
发表于 2025-3-26 17:21:49
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