The advent of treatment modalities with the potential to ameliorate retinal ischemic injury calls for methods allowing their quantitative assessment. We thus established a model of pressure-induced retinal ischemia/reperfusion injury in rats. The intraocular pressure (IOP) was raised to 110 mm Hg by cannulation of the anterior chamber for a duration of 0, 90 or 120 min. The eyes were reperfused for 3 or 7 days. Morphologically, retinal injury occurred in a pattern consistent with retinal and choroidal vascular occlusion. Damage increased in severity with prolonged durations of ischemia. Morphometric determination of the mean thickness of inner retinal layers (MTIRL) revealed significant differences between controls and the 90- or 120-min ischemia groups (p < 0.05 and p < 0.01, respectively). The difference in MTIRL between 3 and 7 days of reperfusion was not significant. Replacement of normal saline by a solution of 5% dextrose in the hydrostatic device used to increase the IOP led to a decrease in retinal injury after 120 min of ischemia (p < 0.01). This model combines a relatively simple methodology, cost-effective execution and a fast, semicomputerized method of quantitation. Depletion of carbohydrates during ischemia may contribute to retinal injury in this model.

In this brief, the utilization of robust model-based predictive control is investigated for the problem of missile interception. Treating the target acceleration as a bounded disturbance, novel guidance law using model predictive control is developed by incorporating missile inside constraints. The combined model predictive approach could be transformed as a constrained quadratic programming (QP) problem, which may be solved using a linear variational inequality-based primal-dual neural network over a finite receding horizon. Online solutions to multiple parametric QP problems are used so that constrained optimal control decisions can be made in real time. Simulation studies are conducted to illustrate the effectiveness and performance of the proposed guidance control law for missile interception.

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