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Design of Control Laws and State Observers for Fixed-Wing UAVs: Simulation Experimental Approaches
Indigo
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Design of Control Laws and State Observers for Fixed-Wing UAVs: Simulation Experimental Approaches
Current price: $176.79
Original price: $221.00


Design of Control Laws and State Observers for Fixed-Wing UAVs: Simulation Experimental Approaches
Current price: $176.79
Original price: $221.00
Loading Inventory...
Size: Kobo eBook
*Product information may vary - to confirm product availability, pricing, shipping and return information please contact Indigo
Design of Control Laws and State Observers for Fixed-Wing UAVs: Simulation and Experimental Approaches provides readers with modeling techniques, simulations, and results from real-time experiments using linear and nonlinear controllers and state observers. The book starts with an overview of the history of UAVs and the equations of motion applied to them. Following chapters analyze linear and nonlinear controllers, state observers, and the book concludes with a chapter discussing testbed development and experimental results, equipping readers with the knowledge they need to conduct their own stable UAV flights whether in simulation or real-time.
Presents aerodynamic models for fixed-wing UAVs that can be used to design control laws and state observers
Applies linear and nonlinear control theories and state observers to fixed-wing UAVs
Provides real-time flight and simulation test results of fixed-wing UAVs with linear and nonlinear controllers
Design of Control Laws and State Observers for Fixed-Wing UAVs: Simulation and Experimental Approaches provides readers with modeling techniques, simulations, and results from real-time experiments using linear and nonlinear controllers and state observers. The book starts with an overview of the history of UAVs and the equations of motion applied to them. Following chapters analyze linear and nonlinear controllers, state observers, and the book concludes with a chapter discussing testbed development and experimental results, equipping readers with the knowledge they need to conduct their own stable UAV flights whether in simulation or real-time.
Presents aerodynamic models for fixed-wing UAVs that can be used to design control laws and state observers
Applies linear and nonlinear control theories and state observers to fixed-wing UAVs
Provides real-time flight and simulation test results of fixed-wing UAVs with linear and nonlinear controllers



















