{"schema_version":"1.0","canonical_url":"https://patentable.app/patents/US-10532829","patent":{"patent_number":"US-10532829","title":"Orbit transfer method for a spacecraft using a continuous or quasi-continuous thrust and embedded driving system for implementing such a method","assignee":null,"inventors":[],"filing_date":"2016-11-09T00:00:00.000Z","publication_date":"2020-01-14T00:00:00.000Z","cpc_codes":["G05D","G01S"],"num_claims":14,"abstract":"An orbit transfer method for a spacecraft using a continuous or quasi-continuous thrust propulsion, the method comprises: the acquisition, at least once in each half-revolution of the spacecraft, of measurements of its position and of its velocity; the computation of a thrust control function as a function of the measurements; and the driving of the thrust in accordance with the control law; wherein the control law is obtained from a Control-Lyapunov function using orbital parameters, preferably equinoctial, of the spacecraft, averaged over at least one half-revolution. An embedded driving system for a spacecraft for implementing such a method and a spacecraft equipped with the driving system are provided."},"analysis":{"summary":null,"layman_explanation":null,"technical_analysis":null,"business_analysis":null,"faqs":null,"topics":[],"tech_cluster":null},"seo":{"title":"Orbit transfer method for a spacecraft using a continuous or quasi-continuous thrust and embedded driving system for implementing such a method","description":"An orbit transfer method for a spacecraft using a continuous or quasi-continuous thrust propulsion, the method comprises: the acquisition, at least once in each half-revolution of the spacecraft, of m","keywords":[]},"attribution":{"source":"Patentable","source_url":"https://patentable.app","canonical_url":"https://patentable.app/patents/US-10532829","license":"CC-BY-4.0-like","license_terms":"AI-generated analysis on this page (summary, layman_explanation, technical_analysis, business_analysis, faqs) may be reused with attribution and a visible link back to the canonical URL above. Patent abstracts, claims, and bibliographic data are USPTO public domain.","required_link":"https://patentable.app/patents/US-10532829","citation_suggestion":"Patentable. \"Orbit transfer method for a spacecraft using a continuous or quasi-continuous thrust and embedded driving system for implementing such a method\" (US-10532829). https://patentable.app/patents/US-10532829","copyright_holder":"Nomic Interactive Technology LLC"},"links":{"html":"https://patentable.app/patents/US-10532829","json":"https://patentable.app/api/llm-context/US-10532829","site":"https://patentable.app","llms_txt":"https://patentable.app/llms.txt"},"generated_at":"2026-05-30T13:43:42.580Z"}