A command model connected to plurality of flight components of an electric aircraft and comprises a circuitry configured to detect a predicted state and a measured state datum, transmit predicted state datum to an actuator model, and transmit measured state datum to a plant model. An actuator model connected to the sensor configured to receive the predicted state datum and generate a performance datum. A plant model connected to the sensor configured to receive measured state datum and performance datum from the actuator model, transmit a feedback path to controller, and generate an inconsistency datum as a function of the measured state datum and the performance datum. A controller communicatively connected to the sensor, wherein the controller is configured to receive the inconsistency datum from the plant model and apply a torque to the aircraft as a function of the inconsistency datum.
SYSTEMS AND METHODS FOR AN AIRCRAFT MOTION OBSERVER IN AN ELECTRIC AIRCRAFT
2023-05-18
Patent
Elektronische Ressource
Englisch
Systems and methods for an aircraft motion observer in an electric aircraft
Europäisches Patentamt | 2022
|Systems and methods for an aircraft motion observer in an electric aircraft
Europäisches Patentamt | 2023
|AIRCRAFT MOTION OBSERVER CONFIGURED FOR USE IN ELECTRIC AIRCRAFT
Europäisches Patentamt | 2022
|