Aerospace Instrument-Making Annotation << Back MULTICRITERIAL DESIGN OF ONBOARD SPACECRAFT CONTROL SYSTEMS D.A. Shelomanov An approach to the design of complex technical systems on the basis of input reserves on the implemented system performance criteria and are considered some of the issues associated with this approach. Criterion of maximizing system performance margin is based on the standard requirements for the characteristics of a complex system, which are, in essence, limiting their values. Each variant of construction of the system, as a rule, the vector of its parameters can be selected to optimize all the characteristics of the system, as different characteristics of the system are determined by the different components of the parameter vector. For example, on-board spacecraft control complex are considered some of the tasks the choice of structure and composition of the system: the number and degree of redundancy of electronic components, the choice of measuring instruments and control. Key words: spacecraft, design, optimization. Contacts: E-mail: sheloman@rambler.ru Pp. 03-10.