Method for inverting earth gravity field of residual inter-star velocity
A technology of gravity and velocity of the earth, which is applied in astronomy, geodynamics, space geodesy, involving the field of satellite gravity, and can solve problems such as complex calculation process and rapid accumulation of dynamic models
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0072] The method of retrieving the earth's gravity field based on the principle of residual interstellar velocity includes the following steps:
[0073] Step 1: Satellite observation data collection
[0074] (1) Obtain the inter-satellite velocity through the space-borne laser interferometric rangefinder Obtain the orbital position of the double satellite through the satellite-borne GPS receiver (r 1 ,r 2 ) and the orbital velocity of the binary star The non-conservative force (f 1 ,f 2 ).
[0075] (2) if figure 1 As shown, using the 9th-order Runge-Kutta linear single-step method and the 12th-order Adams-Cowell linear multi-step numerical simulation formula to obtain the binary star reference orbit position and binary reference orbital velocity
[0076] (3) Reference inter-satellite velocity by reference orbital velocity calculated in, represents the relative reference orbital velocity vector, Indicates the reference unit vector of the first reference ...
Embodiment 2
[0127] Since satellite observations are not independent of each other, they have obvious correlation. Therefore, when retrieving the next-generation GRACE Follow-On Earth's gravity field, correlated colored noise is introduced into the satellite observations.
[0128] The method of retrieving the earth's gravity field based on the principle of residual interstellar velocity includes the following steps:
[0129] Step 1: Satellite observation data collection
[0130] (1) Obtain the inter-satellite velocity through the space-borne laser interferometric rangefinder Obtain the orbital position of the double satellite through the satellite-borne GPS receiver (r 1 ,r 2 ) and the orbital velocity of the binary star The non-conservative force (f 1 ,f 2 ).
[0131] (2) if figure 1 As shown, using the 9th-order Runge-Kutta linear single-step method and the 12th-order Adams-Cowell linear multi-step numerical simulation formula to obtain the binary star reference orbit position ...
PUM
Abstract
Description
Claims
Application Information
- R&D Engineer
- R&D Manager
- IP Professional
- Industry Leading Data Capabilities
- Powerful AI technology
- Patent DNA Extraction
Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.
© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com