ASME 2009 Dynamic Systems and Control Conference, Volume 1 2009
DOI: 10.1115/dscc2009-2787
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Minimization of Degradation Through Prognosis Based Control for a Damaged Aircraft Actuator

Abstract: In this paper we present a formulation of an aircraft systems model for prognosis-based control. An aircraft systems model with hydraulic actuators for control surfaces is developed in SIMULINK and is connected with a model for predicting degradation of an actuator. An LQR based feedback control is employed to compensate for changes in the plant dynamics and a feedforward controller is used to achieve better performance through set-point tracking, while taking into account the current actuator degradation rate… Show more

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Cited by 5 publications
(3 citation statements)
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“…In reality the load on a flight control actuator is depends on many variables related to the dynamics of the aircraft and the desired flight path (for e.g. see Mahulkar et al (2010), Karpenko andSepeheri (2003), andMcCormick (1995)).…”
Section: Mathematical Behavior Modelsmentioning
confidence: 99%
“…In reality the load on a flight control actuator is depends on many variables related to the dynamics of the aircraft and the desired flight path (for e.g. see Mahulkar et al (2010), Karpenko andSepeheri (2003), andMcCormick (1995)).…”
Section: Mathematical Behavior Modelsmentioning
confidence: 99%
“…For this purpose, several strategies have been proposed in the literature. Estimates of degradation of hydraulic actuators were employed in Mahulkar et al (2009) to minimize the degradation rate by means of control strategies with feedforward action. Reference model and reference management strategies were used in Jiang and Zhang (2002) to provide a form of reconfiguration in the event of failures caused by degradation of actuators.…”
Section: Introductionmentioning
confidence: 99%
“…8 In a control perspective, the RUL or other PHM information can be used to compensate for the degradation effects of the actuators by smartly balancing the control effort over them. 2,9,10 This is achieved by reconfiguring the control actions so as to preserve the desired dynamic and static performance of the system, as well as its stability, while protracting the life of the actuators until maintenance operations are carried out.…”
mentioning
confidence: 99%