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Л.Н. Лысенко
20
Ballistic problems in the synthesis of orbital segment
of satellite information system based on small
and micro spacecraft
© L.N. Lysenko
Bauman Moscow State Technical University, Moscow, 105005, Russia
The article presents an analytical review of the major ballistic problems in the synthesis
of orbital segment of satellite information provision system based on small spacecraft.
Much attention is paid to developing the concept of evaluating the possibility of
universalization of small spacecraft satellite system for various purposes. On the basis of
considering the problem statement of the synthesis of a ballistic satellite system structure
as a Pareto-optimal system, it is shown that the small spacecraft system integration is
possible primarily within one class of satellite systems or only “related” satellite system
classes. Taking into consideration the trends in the development of classic heavy samples
of space technology in civilian and dual-purpose systems, the requirements to technology
precision of ballistic-navigation support for satellite system of spacecraft (including
small spacecraft) for various purposes are formulated. The problems of using inter-
satellite navigation and ballistic aspects of the implementation of the inter-satellite
measurement technologies are discussed. The transition from heavy spacecraft systems to
small spacecraft satellite system requires solving totality of innovative problems
associated with both the construction of the individual satellites, and with adaptive
restructuring ballistic-navigation support and its systems
.
Keywords:
satellite system, information provision, small spacecraft, orbital segment syn-
thesis, satellite system structure, system-ballistic characteristics, ballistic-navigation
support, inter-satellite navigation measurements, local group (cluster), innovative tech-
nologies
.
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