Dynamical Model of Rotation and Orbital Coupling for Deimos

This paper introduces a novel dynamical model, building upon the existing dynamical model for Deimos in the current numerical ephemerides, which only encompasses the simple libration effects of Deimos. The study comprehensively incorporates the rotational dynamics of Deimos influenced by the torque...

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Vydáno v:Remote sensing (Basel, Switzerland) Ročník 16; číslo 7; s. 1174
Hlavní autoři: Huang, Kai, Zhang, Lijun, Yang, Yongzhang, Ye, Mao, Li, Yuqiang
Médium: Journal Article
Jazyk:angličtina
Vydáno: Basel MDPI AG 01.04.2024
Témata:
adjustment model
Algorithms
Artificial satellites
Celestial mechanics
Coordinate transformations
Coupling
Deimos
Deimos (Satellite)
Dynamic models
dynamical model
Earth
Ephemerides
Gravitational fields
Gravity
latitude
longitude
Mars
Mathematical models
Methods
Moments of inertia
Moon
Numerical analysis
numerical integration
Observatories
Orbit determination
Orbits
Phobos
Rotation
Solar system
torque
China
United States > US
ISSN:2072-4292, 2072-4292
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Popis
Shrnutí:This paper introduces a novel dynamical model, building upon the existing dynamical model for Deimos in the current numerical ephemerides, which only encompasses the simple libration effects of Deimos. The study comprehensively incorporates the rotational dynamics of Deimos influenced by the torque exerted by the major celestial bodies (Mars, the Sun) in the solar system within the inertial space. Consequently, a full dynamical model is formulated to account for the complete coupling between the rotation and orbit of Deimos. Simultaneously, employing precision orbit determination methods used for artificial satellites, we develop an adjustment model for fitting data to the complete model. The 12-order Adams–Bashforth–Moulton (ABM) integration algorithm is employed to synchronously integrate the 12 state variables of the full model to obtain the orbit of Deimos.The difference in the orbits obtained by integrating the full model over a period of 10 years and those obtained by the simplified model is at the order of 10 km. After precise orbit determination, this difference decreases to below 100 m, so numerical simulation results indicate that the full dynamical model and adjustment model are stable and reliable. Simultaneously, the integration of the Deimos third-order gravity field in the full model over a 10-year period induces only meter-level positional changes. This suggests that when constructing the complete model, the utilization of a second-order gravity field alone is sufficient. Compared to the simple model, the polar axis of Deimos in the inertial space exhibits a more complex oscillation in the full model. Additionally, the full model calculates that the minimum moment of inertia principal axis of Phobos has an amplitude of approximately 0.5 degrees in the longitude direction and does not exceed 2 degrees in the latitude direction. This work further advances the current dynamical model for Deimos and establishes the foundational model for the generation of a new set of precise numerical ephemerides for Deimos.
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ISSN:2072-4292
2072-4292
DOI:10.3390/rs16071174