2019
DOI: 10.2514/1.g004180
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Switching Control Architecture with Parametric Optimization for Aircraft Upset Recovery

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Cited by 8 publications
(3 citation statements)
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References 28 publications
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“…The actions directly affect the training effect of strategies. To quickly change the aircraft state at the initial stage of upset recovery and precisely adjust the aircraft state at the later stage of upset recovery, the action adopted in this study was the deflection change value of the control surface, as shown in Equation (13), where the number of actions was 27, and the thrust was set to 0 to prevent speed exceeding the limit or height loss [17].…”
Section: Actionsmentioning
confidence: 99%
See 1 more Smart Citation
“…The actions directly affect the training effect of strategies. To quickly change the aircraft state at the initial stage of upset recovery and precisely adjust the aircraft state at the later stage of upset recovery, the action adopted in this study was the deflection change value of the control surface, as shown in Equation (13), where the number of actions was 27, and the thrust was set to 0 to prevent speed exceeding the limit or height loss [17].…”
Section: Actionsmentioning
confidence: 99%
“…Dongmo [12] proposed an LOC recovery scheme that combines feedback linearization and high-order sliding mode control. Yildiz [13] proposed a switching control architecture with parametric optimization for aircraft upset recovery. Richards [14] proposed an upset recovery architecture that is applicable to both piloted and autonomous recoveries.…”
Section: Introductionmentioning
confidence: 99%
“…Therefore, ICAO lists the prevention of LOC-I as one of its top safety priorities [1]. In fact, the vast majority of LOC-I accidents are caused by airplane upsets [11]. Therefore, it is very important to study the risk of airplane upsets and explore the risk evolution mechanism for improving flight safety.…”
Section: Introductionmentioning
confidence: 99%