Test automated system of space vehicles automatics and stabilization complexes

Abstract

Automated test system (ATS) design as the separate functionally finished units of a modular design using microprocessor engineering is described. The units of AST are joined by a common control program established on a computer. The suggested construction of ATS will allow, without considerable costs of manufacturing hardware, testing of different automation and stabilisation complexes and of the onboard power supply systems, and deep studies of functionability of similar items.