Analytical solution of the problem on an axisymmetric spacecraft attitude maneuver optimal with respect to a combined functional (Q1982863)
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scientific article; zbMATH DE number 7395311
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Analytical solution of the problem on an axisymmetric spacecraft attitude maneuver optimal with respect to a combined functional |
scientific article; zbMATH DE number 7395311 |
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Analytical solution of the problem on an axisymmetric spacecraft attitude maneuver optimal with respect to a combined functional (English)
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14 September 2021
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Based on the Pontryagin maximum principle for the optimal control problem associated with a spatial attitude maneuver of a spacecraft viewed as a rigid body with one symmetry axis without a constraint on the control function, new analytical solutions are obtained in the classes of conical and generalized conical motions.
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optimal control
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spacecraft
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axisymmetric rigid body
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analytical solution
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0.9145579
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0.9084474
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