Spin-Axis Attitude Determination from Earth Chord-Angle Variations for Geostationary Satellites
Spin stabilization offers a straightforward and robust concept for spacecraft attitude control. The spin-axis attitude determination is usually accomplished by means of sun- and Earth-sensor measurements. This paper explores techniques for spin-axis attitude determination using only Earth-sensor dat...
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| Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 2009-09, Vol.32 (5), p.1598-1608 |
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| container_title | Journal of guidance, control, and dynamics |
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| creator | Van Der Ha, Jozef C Janssens, Frank L |
| description | Spin stabilization offers a straightforward and robust concept for spacecraft attitude control. The spin-axis attitude determination is usually accomplished by means of sun- and Earth-sensor measurements. This paper explores techniques for spin-axis attitude determination using only Earth-sensor data. An immediate attitude determination can be achieved by straightforward geometrical arguments based on the extremes of the chord-angle variations over the orbit Furthermore, an effective least-squares approach is presented that employs a number of equidistant chord-angle measurements collected during one orbital revolution. The adopted measurement model is favorable for reducing the adverse effects of systematic errors. Finally, a few explicit approaches are offered for reconstructing the most important biases. The application of these techniques is illustrated by means of actual telemetry data from the METEOSAT second-generation satellite MSG-2. |
| doi_str_mv | 10.2514/1.40752 |
| format | Article |
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The spin-axis attitude determination is usually accomplished by means of sun- and Earth-sensor measurements. This paper explores techniques for spin-axis attitude determination using only Earth-sensor data. An immediate attitude determination can be achieved by straightforward geometrical arguments based on the extremes of the chord-angle variations over the orbit Furthermore, an effective least-squares approach is presented that employs a number of equidistant chord-angle measurements collected during one orbital revolution. The adopted measurement model is favorable for reducing the adverse effects of systematic errors. Finally, a few explicit approaches are offered for reconstructing the most important biases. 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| ispartof | Journal of guidance, control, and dynamics, 2009-09, Vol.32 (5), p.1598-1608 |
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| language | eng |
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| source | Alma/SFX Local Collection |
| subjects | Accuracy Aeronautics Applied sciences Computer science control theory systems Control theory. Systems Exact sciences and technology Fundamental areas of phenomenology (including applications) Modelling and identification Physics Satellites Sensors Solid dynamics (ballistics, collision, multibody system, stabilization...) Solid mechanics |
| title | Spin-Axis Attitude Determination from Earth Chord-Angle Variations for Geostationary Satellites |
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