Centrala begrepp
Designing a fault-tolerant controller for a Heliquad with full attitude control under actuator failure.
Sammanfattning
The paper presents a Heliquad design with a cambered airfoil propeller for full attitude control under actuator failure. It discusses the theoretical analysis, experimental data, and fault-tolerant control scheme. The content covers VTOL UAV applications, propeller aerodynamics, and neural network-based control allocation.
Statistik
Experimental data shows cambered airfoil propellers generate higher torque.
The maximum tolerable delay in Fault Detection and Isolation (FDI) is 180msec.
Citat
"The cambered airfoil propeller plays a pivotal role in full attitude control under actuator failure."
"Variable Pitch Propellers offer high actuator bandwidth and power optimization."