Phase II: Knowledge Modeling and Computational Intelligence

该小企业创新研究第二阶段项目建议使用第一阶段开发的非线性和线性二次自适应批评算法设计、实施和飞行测试一个基于自适应批评的飞行控制系统；实现了自适应临界飞控系统的硬件在环测试系统；并在精确自动化公司的LoFLYTE神经控制试验台飞机上对自适应临界飞行控制系统进行了飞行测试。

This Small Business Innovation Research Phase II project proposes to design, implement and flight test an adaptive critic based flight control system using both the nonlinear and linear quadratic adaptive critic algorithms developed in Phase I; implement a hardware-in-loop test system for the adaptive critic flight control system; and flight test the adaptive critic flight conotrol system in Accurate Automation's LoFLYTE neurocontrol testbed aircraft.