A Method for Measuring Gravitational Potential of Satellite’s Orbit Using Frequency Signal Transfer Technique between Satellites
نویسندگان
چکیده
We introduce an approach for the direct measurement of gravitational potential (GP) along trajectory a satellite, with specific focus on Low-Earth Orbit (LEO) satellites. A LEO satellite communicates several Geosynchronous Equatorial (GEO) satellites via frequency signal links. The GP difference can be measured in real-time using shift by equipping both and GEO precise atomic clocks. Since at high orbits precisely determined present field model EGM2008, satellite’s determined. In this study, simulation experiments were conducted, featuring GRACE-type as communication three equidistant results indicated that accuracy measurements primarily depends precision onboard Supposing optical clocks attain instability level 1×10−17τ−1/2 (τ seconds), we distribution covered trajectories 30-day observations. Then, centimeter based distribution. data derived from utilized to establish temporal fields, which have broad applications different disciplines.
منابع مشابه
Tracking Control of Uncertain Non - Iinear MIMO System Using Modified Sliding Surfaces for Attitude Large Maneuver of Satellites on Orbit
Designing a robust tracking control for a non-linear MIMO system with uncertainty is one of the most complicated control problems. In this paper, sliding mode changed to non-linear controllable canonical form by input-output linearization. This, sliding surfaces can be defined in a way that we can de-couple equations and indicate the sliding conditions of multi-variable controller system. The u...
متن کاملTracking Control of Uncertain Non - Iinear MIMO System Using Modified Sliding Surfaces for Attitude Large Maneuver of Satellites on Orbit
Designing a robust tracking control for a non-linear MIMO system with uncertainty is one of the most complicated control problems. In this paper, sliding mode changed to non-linear controllable canonical form by input-output linearization. This, sliding surfaces can be defined in a way that we can de-couple equations and indicate the sliding conditions of multi-variable controller system. The u...
متن کاملSatellites measuring `="0200`="003DCO2
Inverse modeling of CO2 sources and sinks using satellite data: A synthetic inter-comparison of measurement techniques and their performance as a function of space and time S. Houweling, F.-M. Breon, I. Aben, C. Rödenbeck, M. Gloor, M. Heimann, and P. Ciais National Institute for Space Research (SRON), Utrecht, The Netherlands Laboratoire des Sciences du Climate et de l’Environnement, Gif sur Y...
متن کاملAn Innovative Method for Measuring Drag on Small Satellites
The need to accurately predict satellite positions is a leading aspect of space situational awareness and presents increased challenges in the specification of the spacecraft environment in low earth orbit. Atmospheric drag is the most important environmental perturbation for low orbiting spacecraft and the most difficult one to model and predict precisely. The author will present a method for ...
متن کاملPrecise Orbit Determination for Low Earth Orbit Satellites
The precise orbit determination problem is to accurately determine the position and velocity vectors of an orbiting satellite. In this paper we review the general contents of the orbit determination process, with particular emphasis on Low Earth Orbit (LEO) satellites. The different orbit determination approaches and the different force models contained within are briefly discussed. The two mai...
متن کاملذخیره 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: ['2072-4292']
DOI: https://doi.org/10.3390/rs15143514