the automated system
rapid navigation-ballistic providing
determination of parameters of motion of space vehicle
In this article from the standpoint of system-technological approach justifies the need to develop a generalized model of technological solutions of ill-posed problem of determining the motion of spacecraft in the implementation of the technological cycle of the operational navigation and ballistic support of spacecraft control. The universality of the proposed solution is based on the paradigm that realizes the principle of invariance with respect to the architecture of an automated system operating the navigation and ballistic software, which is implemented as a template and allows architectural-level synthesis technology to provide the level of model solutions of ill-posed problem of determining the parameters of motion in the form of a set of interfaces (subsystems) , the implementation of which defined a thesaurus methods and algorithms implemented by a specific system.