Abstract:An analysis of current static and time-variable gravity field models is presented focusing on the medium to high frequencies of the geopotential as expressed by the spherical harmonic coefficients. A validation scheme of the gravity field models is implemented based on dynamic orbit determination that is applied in a degree-wise cumulative sense of the individual spherical harmonics. The approach is applied to real data of the Gravity Field and Steady-State Ocean Circulation (GOCE) and Gravity Recovery and Cli… Show more
“…GEORB was released as open source in 2022 [11,12] while preliminary versions of the source code have been developed by Papanikolaou [14,27] for research purposes in topics of satellite geodesy and astrodynamics. The initial focus has been the dynamic orbit analysis of satellite gravity missions GRACE and GOCE aiming at capturing gravity signal discrepancies at orbital altitude through the introduction of a degree-wise cumulative approach of the gravity model contribution [14,28,29].…”
“…GEORB was released as open source in 2022 [11,12] while preliminary versions of the source code have been developed by Papanikolaou [14,27] for research purposes in topics of satellite geodesy and astrodynamics. The initial focus has been the dynamic orbit analysis of satellite gravity missions GRACE and GOCE aiming at capturing gravity signal discrepancies at orbital altitude through the introduction of a degree-wise cumulative approach of the gravity model contribution [14,28,29].…”
“…Typically, spacecraft measure the gravity potential field outside a celestial body, using the Brillouin sphere as a reference point. The Brillouin sphere is the smallest sphere centered at the body’s barycenter that covers all its topography [ 3 ]. Any Doppler ranging or satellite-to-satellite tracking beyond this sphere cannot be used to confidently estimate gravitational potential at altitudes below it.…”
The aim of this work is to create a new type of gravimeter that can function effectively in the challenging conditions of space, specifically on the surfaces of planets and moons. The proposed device, called a diamagnetically stabilized magnetically levitated gravimeter (DSMLG), uses magnetic forces to balance a test mass against the force of gravity, allowing for accurate measurements. A diamagnetically stabilized levitation structure comprises a floating magnet, diamagnetic material, and a lifting magnet. The floating magnet levitates between two diamagnetic plates without the need for external energy input due to the interaction between the magnetic forces of the floating magnet and the stabilizing force of the diamagnetic material. This structure allows for stable levitation of the floating magnet without requiring additional energy. The goal is to design a gravimeter that is lightweight, requires minimal power, can withstand extreme temperatures and shocks, and has a low data rate. The authors envision this gravimeter being used on various robotic spacecraft, such as landers and rovers, to study the interiors of rocky and icy celestial bodies. This paper reports on the results of a finite element model analysis of the DSMLG and the strength of the resulting diamagnetic spring. The findings contribute to the understanding of the levitation characteristics of diamagnetically stabilized structures and provide valuable insights for their practical applications, including in the development of the proposed DSMLG.
“…In recent years, drag-free spacecraft have been successfully used in space missions that require ultra-high stability such as space high-precision earth gravity field surveys [ 1 , 2 , 3 ], space general-relativity verification [ 4 , 5 ], and space gravitational wave detection [ 6 , 7 ]. The success of these missions has greatly encouraged more scholars to research drag-free control systems.…”
This paper proposes a robust control allocation for the capture control of the space inertial sensor’s test mass under overcritical conditions. Uncertainty factors of the test mass control system under the overcritical condition are analyzed first, and a 6-DOF test mass dynamics model with system uncertainty is established. Subsequently, a time-varying weight function is designed to coordinate the allocation of 6-DOF generalized forces. Moreover, a robust control allocation method is proposed to distribute the commanded forces and torques into individual electrodes in an optimal manner, which takes into account the system uncertainties. This method transforms the robust control allocation problem into a second-order cone optimization problem, and its dual problem is introduced to simplify the computational complexity and improve the solving efficiency. Numerical simulation results are presented to illustrate and highlight the fine performance benefits obtained using the proposed robust control allocation method, which improves capture efficiency, increases the security margin and reduces allocation errors.
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