Orbital dynamics of high area-to-mass ratio spacecraft with J2 and solar radiation pressure for novel Earth observation and communication services

This paper investigates the effect of planetary oblateness and solar radiation pressure on the orbits of high area-to-mass spacecraft. A planar Hamiltonian model shows the existence of equilibrium orbits with the orbit apogee pointing towards or away from the Sun. These solutions are numerically continued to non-zero inclinations and considering the obliquity of the ecliptic plane relative to the equator. Quasi-frozen orbits are identified in eccentricity, inclination and the angle between the Sun-line and the orbit perigee. The long-term evolution of these orbits is then verified through numerical integration. A set of ‘heliotropic’ orbits with apogee pointing in the direction of the Sun is proposed for enhancing imaging and telecommunication on the day side of the Earth. The effects of J2 and solar radiation pressure are exploited to obtain a passive rotation of the apsides line following the Sun; moreover the effect of solar radiation pressure enables such orbits at higher eccentricities with respect to the J2 only case.

► Effect of Earth oblateness and solar radiation pressure on orbits of high area-to-mass spacecraft. ► Through planar Hamiltonian find equilibrium orbits with the apse-line passively sun-synchronous. ► Planar solutions numerically continued to non-zero inclinations considering obliquity of ecliptic over the equator. ► Identify quasi-frozen orbits in eccentricity, inclination and angle between Sun-line and perigee. ► Heliotropic orbits with Sun-pointing apogee for enhancing imaging and telecoms on the dayside of the Earth