LEO Satellite Clock Modeling and Its Benefits for LEO Kinematic POD

نویسندگان

چکیده

High-accuracy Low Earth Orbit (LEO) satellite clock and orbital products are preconditions to realize LEO augmentation for high-accuracy GNSS-based positioning on the ground. There is a high correlation between orbit parameters in kinematic Precise Determination (POD) process. While future satellites planned be equipped with better clocks, benefits of modeling high-stability clocks not yet thoroughly investigated, particularly when mid- long-term systematic effects induced by complex relativistic external environment remain clocks. Through modeling, this study attempts reduce only short-term noise radial orbits, but also mis-modeled caused by, e.g., real-time GNSS errors. To explore need first detrended effects. over-detrending limits improvements, weak detrending would hamper strong easily lead performance degradations. A balance strengths model thus needs investigated different types. In study, Piece-Wise Linear (PWL) time lengths 2.5-state filter (h values) tested using real data from GRACE FO-1 an Ultra-Stable Oscillator (USO) board. Using CNES GPS products, it was found that smoothing window 300 500 s, one could generally expect improvement larger than 10% estimation orbits applying PWL length 1200 s. Improvements size can expected h−1 (for Flicker Frequency Noise) 10−28 10−30.

برای دانلود باید عضویت طلایی داشته باشید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Estimation of LEO Satellite

In this paper, we propose a new channel estimation algorithm for low earth orbit satellite digital communications. Low earth orbit satellite channels impart severe spreading in delay and Doppler on the transmitted signal. We model the channel as a tapped-delay-line lter with time-varying complex coeecients. The time evolution of the taps is described by an auto-regressive model. A coupled lter ...

متن کامل

Orbital Perturbation Effect on LEO Satellite Trajectory

A satellite, in its orbit, is affected by perturbing forces, such as atmospheric drag, solar radiation pressure, Earth oblateness, and gravity of the celestial masses (other than the Earth). In this paper, the effects of these forces on the trajectories of different types of LEO satellites and a sample satellite (Z-SAT) are discussed. A few analyses are done on these orbits and the relevant res...

متن کامل

Estimation of LEO Satellite Channels

In this paper, we propose a new channel estimation algorithm for low earth orbit satellite digital communications. Low earth orbit satellite channels impart severe spreading in delay and Doppler on the transmitted signal. We model the channel as a tapped-delay-line lter with time-varying complex coe cients. The time evolution of the taps is described by an auto-regressive model. A coupled lter ...

متن کامل

Routing Issues for Leo Satellite Constellations

We present diierent issues of routing in LEO satellite constellations. The nature of the problem itself needs further explanations. The exact market of these systems lets many questions open, although some models have been advanced. The structure of the ISLs vary from one design to another and impacts signiicantly the optimization. The movement of the satellites also gives to the system a dynam...

متن کامل

Satellite handover techniques for LEO networks

Low earth orbit (LEO) satellite constellations could play an important role in future mobile communication networks due to their characteristics, such as global coverage and low propagation delays. However, because of the non-stationarity of the satellites, a call may be subjected to handovers, which can be cell or satellite handovers. Quite many techniques have been proposed in the literature ...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

ژورنال

عنوان ژورنال: Remote Sensing

سال: 2023

ISSN: ['2315-4632', '2315-4675']

DOI: https://doi.org/10.3390/rs15123149