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Publikováno v:
Unmanned Systems. :1-17
In this paper, a hexarotor Unmanned Aerial Vehicle (UAV) flight dynamics is derived and its control system is designed. A complete mathematical model of the UAV is obtained using Newton–Euler formulation and it is used for simulation. However, a re
Stochastic Estimator Based Adaptive Sliding Mode Control for a Quadrotor in Rainy Flight Conditions.
Publikováno v:
Unmanned Systems; Jan2024, Vol. 12 Issue 1, p133-148, 16p