Researches of planets, interplanetary and circumsolar space give the chance to receive answers to many fundamental questions and to use astronautics achievements by working out of practically unlimited resources of Solar system. Programs of studying of space demand the big material inputs and do not give fast return. Use of perspective electro propulsion systems (EPS) allows raising efficiency of the created and developed space technology. In the decision of a problem of increase scientific and economic efficiency of space researches the important role is played by the complex optimization of mission including definition of optimum structure and parameters of space vehicles (SV) systems, control optimum programs and movement trajectories corresponding to them. Given article is devoted this problem.
Optimal control choice of non-Keplerian orbits with low-thrust propulsion
9TH INTERNATIONAL CONFERENCE ON MATHEMATICAL PROBLEMS IN ENGINEERING, AEROSPACE AND SCIENCES: ICNPAA 2012 ; 2012 ; Vienna, Austria
AIP Conference Proceedings ; 1493 , 1 ; 964-971
2012-11-06
8 pages
Conference paper
Electronic Resource
English
Optimal control choice of non-keplerian orbits with low-thrust propulsion
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