Sampling method and sampling system
US-2024034486-A1 · Feb 1, 2024 · US
US9399528B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9399528-B2 |
| Application number | US-201314093370-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 29, 2013 |
| Priority date | Nov 30, 2012 |
| Publication date | Jul 26, 2016 |
| Grant date | Jul 26, 2016 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A method for stationing a satellite, comprises: determining a predefined trajectory for stationing of the satellite based on a model of movement of the satellite; determining parameters of the predefined control law of approximation of the trajectory and by minimizing impact on the control law of deviation from a trajectory followed by the satellite using parameters of the control law; determining a state vector of the satellite; determining a deviation between the state vector and the predefined trajectory; determining Lagrange multipliers based on a current state vector of the satellite, on a deviation between current state vector and predefined trajectory and on parameters of the predefined control law; determining parameters of the current control law of the engines based on the Lagrange multipliers and by derivation of a parameter representative of an effect of engines on the real trajectory; and controlling engines based on parameters of the current control law.
Opening claim text (preview).
The invention claimed is: 1. A method for stationing a satellite, characterized in that it comprises: a first step of determining a predefined trajectory used for said stationing of said satellite based on a model of movement of said satellite; a second step of determining parameters of a predefined control law of approximation of said predefined trajectory and minimizing an impact of said predefined control law on a deviation from a real trajectory followed by said satellite us…
Operations & Transport · mapped topic
Operations & Transport · mapped topic
Operations & Transport · mapped topic
Operations & Transport · mapped topic
Physics · mapped topic
Related publications grouped by family.
Free tools are coming soon. Tell us what you want to track and we'll notify you.
Answers are generated from the same data shown on this page.