Quaternion methods and regular models of celestial and space flight mechanic: using Euler (Rodrigues-Hamilton) parameters to describe orbital (trajectory) motion. II: Perturbed spatial restricted three-body problem (Q2699160)
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| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Quaternion methods and regular models of celestial and space flight mechanic: using Euler (Rodrigues-Hamilton) parameters to describe orbital (trajectory) motion. II: Perturbed spatial restricted three-body problem |
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Statements
Quaternion methods and regular models of celestial and space flight mechanic: using Euler (Rodrigues-Hamilton) parameters to describe orbital (trajectory) motion. II: Perturbed spatial restricted three-body problem (English)
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26 April 2023
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perturbed spatial restricted three-body problem
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regular quaternion models
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Euler (Rodrigues-Hamilton) parameters
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Hamilton rotation quaternion
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spacecraft
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nonholonomic
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orbital and ideal coordinate systems
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