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- W4236023566 abstract "This chapter presents the detailed dynamic model of a Vertical Take-Off and Landing (VTOL) type Unmanned Aerial Vehicle (UAV) known as the quadrotor. The mathematical model is derived based on Newton Euler formalism. This is followed by the development of a simulation environment on which the developed model is verified. Four control algorithms are developed to control the quadrotor's degrees of freedom: a linear PID controller, Gain Scheduling-based PID controller, nonlinear Sliding Mode, and Backstepping controllers. The performances of these controllers are compared through the developed simulation environment in terms of their dynamic performance, stability, and the effect of possible disturbances." @default.
- W4236023566 created "2022-05-12" @default.
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- W4236023566 date "2019-01-01" @default.
- W4236023566 modified "2023-10-16" @default.
- W4236023566 title "Dynamic Modeling and Control Techniques for a Quadrotor" @default.
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- W4236023566 doi "https://doi.org/10.4018/978-1-5225-8365-3.ch002" @default.
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