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| SGP4 TLE-propagaatio× | B-Dot-säädin× | |
|---|---|---|
| Tieteenala | Ilmailu- ja avaruustekniikka | Ilmailu- ja avaruustekniikka |
| Menetelmäperhe | Process / pipeline | Process / pipeline |
| Syntyvuosi≠ | 1970s | 1980s |
| Kehittäjä≠ | NORAD, USAF | Spacecraft attitude control engineers |
| Tyyppi≠ | Propagation method | Control law |
| Alkuperäislähde≠ | Vallado, D. A., Crawford, P., Hujsa, R., & Kelso, T. S. (2006). Revisiting Spacetrack Report Number 3. In AIAA/AAS Astrodynamics Specialist Conference. DOI ↗ | Wertz, J. R. (Ed.). (2002). Spacecraft Attitude Determination and Control. Kluwer Academic. link ↗ |
| Rinnakkaisnimet | SGP4, TLE propagation, simplified perturbations | B-dot control, magnetic damping, momentum dumping |
| Liittyvät | 3 | 3 |
| Tiivistelmä≠ | SGP4 (Simplified General Perturbations 4) is a rapid orbital propagation method that predicts satellite position and velocity from Two-Line Element (TLE) sets published by NORAD. Developed in the 1970s, SGP4 accounts for atmospheric drag, gravitational perturbations, and solar radiation pressure using simplified analytical models. SGP4 is the de facto standard for space surveillance, conjunction assessment, and satellite tracking. | The B-Dot controller (magnetic B-dot control law) is a simple, robust spacecraft attitude control method that uses the rate of change of Earth's magnetic field measured onboard to generate a magnetic dipole moment. Developed in the 1980s, the B-Dot law damps spacecraft angular momentum without requiring a complex attitude estimate or external reference, making it ideal for initial momentum dumping after launch or in contingency scenarios. B-Dot is passive, simple to implement, and effective. |
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