TY - BOOK ID - 7837536 TI - Fault Tolerant Control Schemes Using Integral Sliding Modes AU - Hamayun, Mirza Tariq. AU - Edwards, Christopher. AU - Alwi, Halim. PY - 2016 SN - 3319322362 3319322389 PB - Cham : Springer International Publishing : Imprint: Springer, DB - UniCat KW - Mechanical Engineering - General KW - Mechanical Engineering KW - Engineering & Applied Sciences KW - Sliding mode control. KW - Fault tolerance (Engineering) KW - Fault tolerant design KW - Fault withstandability (Engineering) KW - Reliability (Engineering) KW - Automatic control KW - Systems theory. KW - Control and Systems Theory. KW - Systems Theory, Control. KW - Control engineering. KW - System theory. KW - Systems, Theory of KW - Systems science KW - Science KW - Control engineering KW - Control equipment KW - Control theory KW - Engineering instruments KW - Automation KW - Programmable controllers KW - Philosophy UR - https://www.unicat.be/uniCat?func=search&query=sysid:7837536 AB - The key attribute of a Fault Tolerant Control (FTC) system is its ability to maintain overall system stability and acceptable performance in the face of faults and failures within the feedback system. In this book Integral Sliding Mode (ISM) Control Allocation (CA) schemes for FTC are described, which have the potential to maintain close to nominal fault-free performance (for the entire system response), in the face of actuator faults and even complete failures of certain actuators. Broadly an ISM controller based around a model of the plant with the aim of creating a nonlinear fault tolerant feedback controller whose closed-loop performance is established during the design process. The second approach involves retro-fitting an ISM scheme to an existing feedback controller to introduce fault tolerance. This may be advantageous from an industrial perspective, because fault tolerance can be introduced without changing the existing control loops. A high fidelity benchmark model of a large transport aircraft is used to demonstrate the efficacy of the FTC schemes. In particular a scheme based on an LPV representation has been implemented and tested on a motion flight simulator. ER -