A Way for Accelerated Calculation of Spacecraft Motion in an Atmosphere with a Tethered Aerodynamic Stabilizer

摘要

A method for rapid calculation of spacecraft (SC) motion in the atmosphere with a teth-ered aerodynamic stabilizer (AS) is presented. The core of the method consists of artificially increasing the oscillation period, which makes it possible to substantially reduce both the laboriousness of the cal-culations and the computation error that influences the accuracy of the integration. The algorithm for choosing the magnification coefficient for the oscillation period is presented.