An approximate solution of the equations of motion for arbitrary rotating spacecraft / by Peter R. Kurzhals.
The assumption of small changes in the inertia parameters has been used to derive approximate rotational equations of motion for arbitrary spinning spacecraft in the small angle and rate regime. Complex representations are introduced to define the rate and attitude errors produced by applied disturb...
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| Corporate Authors: | , |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Aeronautics and Space Administration,
[1967]
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| Series: | NASA technical report ;
R-269. |
| Subjects: |
Norlin Library - Government Information - US
| Call Number: |
NAS 1.12:269
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| NAS 1.12:269 | Available Place a Hold |