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- W209835651 abstract "In the last decades a number of countries have shown interest towards anti-satellitesystems for strategic military purposes. In general, anti-satellite weapons are employedto intercept and destroy adversary or malfunctioning satellites. This study is concernedwith the determination of the optimal, i.e. minimum{time trajectories leading to the in-terception of low Earth satellites by a ground{launched interceptor, which is representedby a two{stage rocket. The target satellite is assumed to be placed in a repeating groundtrack orbit, so the performance of the anti-satellite interceptor can be evaluated overthe period of repetition of the repeating orbit. This paper addresses the additional opti-mization problem of determining the geographical regions where the launch site can belocated so that interception can occur in a speci¯ed time. The numerical solutions arederived through the use of a direct optimization method, termed direct collocation withnonlinear programming.[ DOI : 10.1685/CSC09265] About DOI" @default.
- W209835651 created "2016-06-24" @default.
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- W209835651 date "2009-08-12" @default.
- W209835651 modified "2023-09-28" @default.
- W209835651 title "Optimal Trajectories of Anti-Satellite Missiles" @default.
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