Fourth-order gravity gradient torque of spacecraft orbiting asteroids
Yue Wang, Hong Guan, Shijie Xu

TL;DR
This paper develops a more accurate fourth-order gravity gradient torque model for spacecraft orbiting irregularly shaped asteroids by including higher-order inertia integrals, verified through numerical simulations.
Contribution
The paper introduces a full fourth-order gravity gradient torque model considering higher-order inertia integrals, improving accuracy over previous models for spacecraft around non-spherical asteroids.
Findings
The new model closely matches exact motion in simulations.
Previous models showed significant deviations from actual motion.
The model is suitable for practical mission design applications.
Abstract
The dynamical behavior of spacecraft around asteroids is a key element in design of such missions. An asteroid's irregular shape, non-spherical mass distribution and its rotational sate make the dynamics of spacecraft quite complex. This paper focuses on the gravity gradient torque of spacecraft around non-spherical asteroids. The gravity field of the asteroid is approximated as a 2nd degree and order-gravity field with harmonic coefficients C20 and C22. By introducing the spacecraft's higher-order inertia integrals, a full fourth-order gravity gradient torque model of the spacecraft is established through the gravitational potential derivatives. Our full fourth-order model is more precise than previous fourth-order model due to the consideration of higher-order inertia integrals of the spacecraft. Some interesting conclusions about the gravity gradient torque model are reached. Then a…
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Taxonomy
TopicsAstro and Planetary Science · Planetary Science and Exploration · Geomagnetism and Paleomagnetism Studies
