Automation of Calculation and Analysis of Dynamic Characteristics of Launch Vehicles Constructions

Problems are discussed of automation of the initial data preparation for the stabilization system development in design of construction dynamics taking into account the adaptation of space-purpose rockets for launch of various spacecrafts. The program-mathematic complex is described which allows the effective solution of these problems. A typical scheme of calculation and analysis of dynamic characteristics of space-purpose rockets using the given complex is presented. Possibilities of the complex application for the analysis of the closed system "object-regulator" and the post-flight analysis of telemetry data are considered.