The analysis of efficiency of satellte inspectors with electrojet impellent modules

In work the technique of an estimation of efficiency of satellite inspectors equipped electrojet impellent modules is considered. The general problem of systems multicriteria optimization is formulated. The dynamic problem of management by elements of an orbit and relative movement is allocated and the technique of its decision is offered. The procedure of calculation propulsive masss reserve guaranteeing performance of set of operations of rapprochement with inspected object is offered. The algorithm of a choice of the basic design parameters of the satellite inspector with electrojet impellent module is described.