supported by the National Basic Research Program(973Program)(2015CB755805);the National Natural Science Foundation of China(61374145)
To solve the flight safety problem caused by nonlinear instabilities(category II pilot induced oscillations, PIOs) of the closed-loop pilot-vehicle system with rate-limiting actuator, the antiwindup(AW) compensati...
supported by the National Natural Science Foundation of China(Nos.61174073,90816028)
This paper investigates the stability analysis and antiwindup design problem for a class of discrete-time switched linear systems with time-varying norm-bounded uncertainties and saturating actuators by using the swit...