Optimal injection of a satellite into geostationary orbit using a limited number of thruster firings (Q2017634)

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scientific article; zbMATH DE number 6418201
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English
Optimal injection of a satellite into geostationary orbit using a limited number of thruster firings
scientific article; zbMATH DE number 6418201

    Statements

    Optimal injection of a satellite into geostationary orbit using a limited number of thruster firings (English)
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    23 March 2015
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    optimal injection
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    satellite
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    geostationary orbit
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    continuous-discrete system
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    necessary optimality conditions
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