Approaches to optimizing guidance methods to high-speed intensively maneuvering targets. Part II. Analyzing the capabilities of different ways to optimize guidance methods

Based on the requirements for optimization methods of high-speed aircraft interception systems (see part I of the study), different ways to optimize guidance methods are analyzed. The capabilities of the classical theory of optimal control, as well as its modifications with local optimization and local optimization by the minimum of quadratic-biquadratic performance functionals, are considered at the qualitative level within the concept of inverse dynamics problems. In addition, the ways to optimize the information support of all approaches are assessed.