![]() ![]() Instructor direct assessment and student formal feedback demonstrate that active and experiential learning methodologies using numerical simulation are received positively by students and prove to be effective in increasing student motivation and participation and generally enhancing the academic process. The general design and implementation of the assignment employs active and experiential learning approaches and promotes student initiative and creativity. The students receive general guidelines on how to design and execute the simulation experiment however, they are required to answer open-ended questions and encouraged to investigate and follow personal paths in reaching the objective of the assignment. The main objective of the lab consists in capturing the dynamic fingerprint of actuator failure as a necessary premise for the development of fault tolerant control laws and schemes for subsystem failure detection, identification, and evaluation. They can be locked at trim or at a different deflection. The typical aircraft aerodynamic control surfaces are targeted in the assignment: aileron, elevator, and rudder. The computational package relies on Matlab ® and Simulink ®. Advanced simulation tools are used to illustrate concepts and allow students to identify the dynamic fingerprint of aircraft actuator failures and investigate qualitatively their effects on system performance and handling qualities. However, the laboratory assignment can be a valuable addition to other courses in flight dynamics and controls. The laboratory was developed in the context of introducing aerospace engineering students to the practical implications of subsystem malfunctions on aircraft dynamics, performance, and control within the general framework of aircraft health management. ![]() The design and implementation of an undergraduate laboratory is presented for the analysis of aircraft actuator failures through simulation. ![]()
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