Precise Solar Radiation Pressure Models for Small-Body Orbiters: Applications to OSIRIS-REx Spacecraft

This paper presents a framework for the precise representation of solar radiation pressure effects on spacecraft orbiting around small bodies. It uses a Fourier-series expansion to model the solar radiation force that is imparted on the spacecraft. A set of dominant Fourier coefficients that account...

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Veröffentlicht in:	Journal of guidance, control, and dynamics control, and dynamics, 2017-07, Vol.40 (7), p.1638-1650
Hauptverfasser:	Hesar, Siamak G, Scheeres, Daniel J, McMahon, Jay W
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerospace engineering Apollo asteroids Asteroid missions Asteroids Coefficients Covariance Error analysis Exact solutions Feasibility studies Fourier analysis Fourier series Global positioning systems GPS Mathematical models Methods Numerical analysis Orbits Origins Pressure effects Radiation Radiation pressure Regolith Satellites Security Series expansion Solar radiation Spacecraft Spacecraft orbits Spectra Uncertainty Uncertainty analysis
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