The importance of NADPH oxidase (Nox) in hypoxic responses in hypoxia-sensing cells, including pulmonary artery smooth muscle cells (PASMCs), remains uncertain. In this study, using Western blot analysis we found that the major Nox subunits Nox1, Nox4, p22(phox), p47(phox), and p67(phox) were equivalently expressed in mouse pulmonary and systemic (mesenteric) arteries. However, acute hypoxia significantly increased Nox activity and translocation of p47(phox) protein to the plasma membrane in pulmonary, but not mesenteric, arteries. The Nox inhibitor apocynin and p47(phox) gene deletion attenuated the hypoxic increase in intracellular concentrations of reactive oxygen species and Ca(2+) ([ROS](i) and [Ca(2+)](i)), as well as contractions in mouse PASMCs, and abolished the hypoxic activation of Nox in pulmonary arteries. The conventional/novel protein kinase C (PKC) inhibitor chelerythrine, specific PKCepsilon translocation peptide inhibitor, and PKCepsilon gene deletion, but not the conventional PKC inhibitor GO6976, prevented the hypoxic increase in Nox activity in pulmonary arteries and [ROS](i) in PASMCs. The PKC activator phorbol 12-myristate 13-acetate could increase Nox activity in pulmonary and mesenteric arteries. Inhibition of mitochondrial ROS generation with rotenone or myxothiazol prevented hypoxic activation of Nox. Glutathione peroxidase-1 (Gpx1) gene overexpression to enhance H(2)O(2) removal significantly inhibited the hypoxic activation of Nox, whereas Gpx1 gene deletion had the opposite effect. Exogenous H(2)O(2) increased Nox activity in pulmonary and mesenteric arteries. These findings suggest that acute hypoxia may distinctively activate Nox to increase [ROS](i) through the mitochondrial ROS-PKCepsilon signaling axis, providing a positive feedback mechanism to contribute to the hypoxic increase in [ROS](i) and [Ca(2+)](i) as well as contraction in PASMCs.

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To estimate the flight attitude angles of Guided Projectile rapidly and accurately to realize the precise control, angular motion equations and MEMS gyroscope measurements were used to build the state equation and the measurement equationcombined withthe ballistic priori knowledge. Based on the unscented kalman filter for nonlinear system, an approach of estimating the attitude angles of Guided Projectile was proposed. Taking a certain type of Guided Projectile as an example, the data of triaxial angular velocities with the measurement noise was considered as the output signal of MEMS gyros, and considered the calculated ballistic data as the ballistic priori knowledge. Through the approach proposed in this paper, the above were used to obtain the estimates for attitude angles. The results indicate that, it’s feasible to obtain the attitude angles by angular motion equations and gyros. On account of the actual random noise signal of gyros, the accuracy of the estimated attitude angles can meet the requirement of trajectory control system for Guided Projectile.