SIMULATION OF THE CONTROL PROCESSES OF THE AUTOMATIC SPACECRAFT FOR OBSERVATION IN THE REGIMES OF THE TARGET FUNCTIONING
Alexander Kucherov, Vladimir Kurenkov, Vadim Salmin
In the process of automatic spacecraft (AS) design it is necessary to estimate the characteristics of space system target effectiveness depending on such the factors, as parameters of AS orbital flight, operating condition, supply system design characteristics, onboard service systems actigrams and others. The bundled software have been developed under Delphi-7 environment in order to solve the problem. It has user-friendly interface and can be exploited even by inexperienced users.