METHOD OF CALCULATING THE DESCENT OF THE SPACECRAFT IN THE ATMOSPHERE USING TECHNOLOGY ADAPTATION LANDING IN DIFFERENT ENVIRONMENTAL CONDITIONS

摘要

The paper presents a method of calculating the parameters of angular motion landing vehicle, based on joint integration of the differential equations of motion and partial differential equations describing the change in the form of an inflatable braking device during descent vehicle in the atmosphere. Shown the results of modeling the movement of the landing vehicle with inflatable braking device. Shown that the main factor causing the change in the parameters of angular motion landing vehicle, is the asymmetry of external form.