{"schema_version":"1.0","canonical_url":"https://patentable.app/patents/US-11970281","patent":{"patent_number":"US-11970281","title":"Integrated feedback to flight computer for adjusting power distribution to rotorcraft motors","assignee":null,"inventors":[],"filing_date":"2020-07-14T00:00:00.000Z","publication_date":"2024-04-30T00:00:00.000Z","cpc_codes":["G05D","G05D"],"num_claims":20,"abstract":"A method and system for providing corrective action to a rotorcraft experiencing motor failure is provided. Included in the method and system are embodiments that receive feedback from sensors directed at measuring a state of motors used to provide lift to the rotorcraft. The method and system also describe embodiments for determining that there is a malfunctioning motor, and furthermore, the appropriate corrective action for responding to the malfunctioning motor. In some embodiments, the method and system are configured to reduce power to the malfunctioning motor while simultaneously adjusting power supplied to the remaining motors such that changes in total thrust and net torque are minimized. Further, the method and system are configured to perform diagnostics on the malfunctioning motor while power is still being supplied to the first motor."},"analysis":{"summary":null,"layman_explanation":null,"technical_analysis":null,"business_analysis":null,"faqs":null,"topics":[],"tech_cluster":null},"seo":{"title":"Integrated feedback to flight computer for adjusting power distribution to rotorcraft motors","description":"A method and system for providing corrective action to a rotorcraft experiencing motor failure is provided. Included in the method and system are embodiments that receive feedback from sensors directe","keywords":[]},"attribution":{"source":"Patentable","source_url":"https://patentable.app","canonical_url":"https://patentable.app/patents/US-11970281","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-11970281","citation_suggestion":"Patentable. \"Integrated feedback to flight computer for adjusting power distribution to rotorcraft motors\" (US-11970281). https://patentable.app/patents/US-11970281","copyright_holder":"Nomic Interactive Technology LLC"},"links":{"html":"https://patentable.app/patents/US-11970281","json":"https://patentable.app/api/llm-context/US-11970281","site":"https://patentable.app","llms_txt":"https://patentable.app/llms.txt"},"generated_at":"2026-05-31T08:34:20.619Z"}