摘要: This research is designed to demonstrate that a change in satellite propellant can be determined using measured moments of inertia (MOI) from a satellite. Because satellites are currently incapable of being refueled in orbit it is... 展开
作者 | Geitgey, J. W. | ||
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原报告号 | ADA453964 | 总页数 | 163 |
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Orbits Spacecraft Least squares method Moment of inertia Mathematical models Detection Parameters Accuracy Estimates Fuels Response Selection Operators(Personnel) Telemetering data Calibration Maneuvers Artificial satellites Base lines Propellants Theses Dynamic response Models Air force Simulation |