Design and optimization on trajectory of increasing velocity along its original velocity direction by impulse firing for ballistic missile to penetrate anti-missile system in passive ballistic curve

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作者
Zhang, Bin [1 ]
Ren, Junxue [1 ]
Wang, Yibai [1 ]
Liu, Yu [1 ]
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[1] School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
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页码:650 / 653
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  • [2] The method of the impulse trajectory transfer in a plane for the ballistic missile breaking through a defense line in the passive ballistic curve
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