Systems and methods for reducing aircraft load
The aircraft flight control system addresses load-related challenges by optimizing flight configurations and managing aerodynamic loads, enhancing safety and efficiency through sensor-driven effector commands.
JP2026518454APending Publication Date: 2026-06-08ARCHER AVIATION INC
Patent Information
- Authority / Receiving Office
- JP · JP
- Patent Type
- Applications
- Current Assignee / Owner
- ARCHER AVIATION INC
- Filing Date
- 2024-05-29
- Publication Date
- 2026-06-08
Smart Images
Figure 2026518454000001_ABST
Abstract
Aspects of the present disclosure generally relate to systems and methods for flight control of aircraft driven by electric propulsion systems and other types of vehicles. In some embodiments, an aircraft flight control system is configured to receive one or more signals for controlling the motion of an aircraft, determine at least one flight condition of the aircraft including at least one flight phase, calculate at least one load associated with the aircraft based on the determined at least one flight condition, determine an optimized flight configuration to reduce the load on one or more components of the aircraft based on the received one or more signals and the calculated loads, generate one or more effector commands based on the optimized flight configuration, and activate one or more aircraft effectors based on the one or more effector commands.
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