Methods for attitude & orbit control of the information satellites with economical expending of the energy and fuel onboard resources are presented. We consider the land-survey mini-satellites with orbital altitude from 600 up to 800 km when their lifetime must be up to 10 years and economical control is actual problem. We also consider the optimization problems on attitude guidance of such spacecraft, discrete filtering of measured signals, economical control with respect to the onboard energy and fuel resources and present elaborated methods for their solving.


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    Title :

    Optimization of guidance and attitude control for land-survey mini-satellites


    Contributors:

    Conference:

    10TH INTERNATIONAL CONFERENCE ON MATHEMATICAL PROBLEMS IN ENGINEERING, AEROSPACE AND SCIENCES: ICNPAA 2014 ; 2014 ; Narvik, Norway


    Published in:

    AIP Conference Proceedings ; 1637 , 1 ; 1018-1027


    Publication date :

    2014-12-10


    Size :

    10 pages





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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