摘要
概要地介绍了具有冗余操纵面的飞控系统中受限控制量分配问题的概念、数学表述方法和直接最优分配方案及其几何算法，并指出该算法存在难于计算机实现的困难。通过分析，将该问题转化为标准线性规划问题，给出了详细的转化过程，从而使其易于计算机实现。最后通过算例说明了这种改进和算法是正确有效的。
In this paper, the concept about constrained control allocation in the flight control systems and its mathematical description are simply introduced. The program of direct optimal allocation and its geometrical calculation method is also introduced. It is indicated that the realization of this algorithm on computer is difficulty. By analysing, this method is transformed to the linear programming problem, and the transforming procedure is provided. The linear programming problem should be easily solved on computer. Finally, the method is shown to be correct and effective by an example.
出处
《飞行力学》
CSCD
北大核心
1999年第2期41-45,共5页
Flight Dynamics
