Optimal spatial launch of a spacecraft into a geostationary orbit from and artificial satellite orbit (Q1901547)
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scientific article; zbMATH DE number 817411
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Optimal spatial launch of a spacecraft into a geostationary orbit from and artificial satellite orbit |
scientific article; zbMATH DE number 817411 |
Statements
Optimal spatial launch of a spacecraft into a geostationary orbit from and artificial satellite orbit (English)
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7 January 1996
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thrust vector
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central Newtonian field
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maximum principle
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boundary value problem
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0.90386087
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0.87710744
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0.8710766
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0.85393775
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0.8464354
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0.84554195
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0.8440968
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0.83887255
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0.83874655
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