Apurine/pyrimidine-free endonuclease 1(APEX1)is a multifunctional enzyme that contributes to oxidization-mediated DNA-cleaved base excision repair and redox activation of transcription factors.However,the role of APEX...Apurine/pyrimidine-free endonuclease 1(APEX1)is a multifunctional enzyme that contributes to oxidization-mediated DNA-cleaved base excision repair and redox activation of transcription factors.However,the role of APEX1 during cardiomyocyte oxidative stress injury is not completely understood.In the present study,whether APEX1 protects oxidative damage-induced cardiomyocytes was investigated.mRNA and protein expression levels of APEX1 were downregulated in the mouse model of cardiac ischemia-reperfusion injury.Furthermore,the expression of APEX1 in hydrogen peroxide(H 2 O 2)-treated neonatal mice cardiomyocytes was also decreased.APEX1 knockdown aggravated H 2 O 2-treated cardiomyocyte apoptosis indexes.By contrast,APEX1 overexpression reversed H 2 O 2-induced oxidative damage,as demonstrated by decreased caspase 3 and Bax expression levels.Moreover,homeobox A5 upregulated APEX1.The results of the present study indicated that APEX1 displayed protective effects against oxidative damage,suggesting that APEX1 may serve as a unique protective strategy for cardiac ischemia-reperfusion injury.展开更多
This paper addresses the three-dimensional(3-D)approach angle constrained cooperative guidance problem for speed-varying missiles against maneuvering targets.First,the guidance problem is formulated in a relative refe...This paper addresses the three-dimensional(3-D)approach angle constrained cooperative guidance problem for speed-varying missiles against maneuvering targets.First,the guidance problem is formulated in a relative reference frame and a virtual control input is selected.Then,the cooperative guidance law is designed on the basis of a prediction-correction framework.The time-to-go under the baseline command is estimated by an efficient prediction method with a realistic aerodynamic model and a biased command is developed by utilizing the time-to-go predictions for synchronizing different missiles'impact times.The design of the biased command is decoupled into the individual design of its direction and magnitude.It is proved that the designed cooperative guidance law can make the time-to-go consensus error converge to zero before interception.Finally,the designed guidance law is validated through a series of numerical simulations.展开更多
基金supported by the National Natural Science Foundation of China(Grant No.81900245 and 81770395).
文摘Apurine/pyrimidine-free endonuclease 1(APEX1)is a multifunctional enzyme that contributes to oxidization-mediated DNA-cleaved base excision repair and redox activation of transcription factors.However,the role of APEX1 during cardiomyocyte oxidative stress injury is not completely understood.In the present study,whether APEX1 protects oxidative damage-induced cardiomyocytes was investigated.mRNA and protein expression levels of APEX1 were downregulated in the mouse model of cardiac ischemia-reperfusion injury.Furthermore,the expression of APEX1 in hydrogen peroxide(H 2 O 2)-treated neonatal mice cardiomyocytes was also decreased.APEX1 knockdown aggravated H 2 O 2-treated cardiomyocyte apoptosis indexes.By contrast,APEX1 overexpression reversed H 2 O 2-induced oxidative damage,as demonstrated by decreased caspase 3 and Bax expression levels.Moreover,homeobox A5 upregulated APEX1.The results of the present study indicated that APEX1 displayed protective effects against oxidative damage,suggesting that APEX1 may serve as a unique protective strategy for cardiac ischemia-reperfusion injury.
基金supported by Key R&D Program(Soft Science Project)of Shandong Province,China(No.2020CXGC011502)National Natural Science Foundation of China(Nos.62273043 and 62103049).
文摘This paper addresses the three-dimensional(3-D)approach angle constrained cooperative guidance problem for speed-varying missiles against maneuvering targets.First,the guidance problem is formulated in a relative reference frame and a virtual control input is selected.Then,the cooperative guidance law is designed on the basis of a prediction-correction framework.The time-to-go under the baseline command is estimated by an efficient prediction method with a realistic aerodynamic model and a biased command is developed by utilizing the time-to-go predictions for synchronizing different missiles'impact times.The design of the biased command is decoupled into the individual design of its direction and magnitude.It is proved that the designed cooperative guidance law can make the time-to-go consensus error converge to zero before interception.Finally,the designed guidance law is validated through a series of numerical simulations.
