“…The output from the Min-Max algorithm is the fuel flow rate signal that causes that the thrust command will be provided, and none of the operational and safety limits will be violated (Decastro et al, 2008; Garg, 2013; Jaw and Mattingly, 2009; Litt et al, 2009; Montazeri-Gh and Jafari, 2011; Spang and Brown, 1999). In addition to aircraft engine, the Min-Max selector control scheme can be used to control many other constrained systems such as industrial gas turbine engines (Mohammadi and Montazeri-Gh, 2016), distillation towers for temperature control (Oglesby, 1996), Anti-Windup systems (Kothare and Morari, 1999), electric motors, power industry for control of boilers, power systems, and nuclear reactors (Glattfelder and Schaufelberger, 2003).…”