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- W2145893156 abstract "The dynamical modeling of an Unmanned Air Vehicle (UAV) forms the heart of its simulation. The equations of motion can take five different forms: 1) nonlinear fully coupled, 2) nonlinear semi-coupled, 3) nonlinear decoupled, 4) linear coupled, and 5) linear decoupled. In the fully coupled equations of motion, two new coupling stability derivatives ( ! D C , ! L C ) are incorporated. The main purpose of this paper is to compare each version of the equations of motion, and to demonstrate positive and negative features of each form. This paper also compares the five different dynamical models using eight distinct UAV missions. It analyzes them from three different aspects, and gives recommendations for which model is best for a specified mission. MATLAB/Simulink is used to implementation the simulation. The final results are compared by analyzing the resulting trajectories and control deflections." @default.
- W2145893156 created "2016-06-24" @default.
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- W2145893156 date "2005-06-19" @default.
- W2145893156 modified "2023-09-27" @default.
- W2145893156 title "UAV Flight Simulation: Credibility of Linear Decoupled vs. Nonlinear Coupled Equations of Motion" @default.
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- W2145893156 doi "https://doi.org/10.2514/6.2005-6425" @default.
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