US 12,393,199 B2
Methods and systems for a distributed control system with supplemental attitude adjustment
Herman Wiegman, South Burlington, VT (US)
Assigned to BETA AIR LLC, South Burlington, VT (US)
Filed by BETA AIR, LLC, South Burlington, VT (US)
Filed on May 31, 2023, as Appl. No. 18/203,742.
Application 18/203,742 is a continuation in part of application No. 17/949,816, filed on Sep. 21, 2022, granted, now 11,714,427.
Application 17/949,816 is a continuation of application No. 17/526,499, filed on Nov. 15, 2021, granted, now 11,467,606, issued on Oct. 11, 2022.
Prior Publication US 2024/0004404 A1, Jan. 4, 2024
Int. Cl. B64C 13/00 (2006.01); B64C 13/04 (2006.01); G05D 1/00 (2006.01)
CPC G05D 1/085 (2013.01) [B64C 13/0421 (2018.01); G05D 1/042 (2013.01); G05D 1/0607 (2013.01)] 20 Claims
OG exemplary drawing
 
1. A distributed control system with supplemental attitude adjustment, the system comprising:
an aircraft control;
a plurality of flight components attached to an aircraft, wherein the aircraft has an aircraft attitude;
a plurality of aircraft components communicatively connected to the plurality of flight components, wherein each aircraft component of the plurality of aircraft components is configured to:
receive, from a command sensor attached to the aircraft control, an aircraft command; and
generate a response command directing the flight components as a function of a supplemental attitude and the aircraft attitude, wherein the response command comprises a trim adjustment.