CPC G05D 1/102 (2013.01) [B64C 29/00 (2013.01); B64D 27/24 (2013.01)] | 20 Claims |
1. A system for scaling lag based on flight phase of an electric aircraft, the system comprising:
a sensor communicatively connected to an electric vertical takeoff and landing (eVTOL) aircraft, wherein the sensor is configured to:
detect measured aircraft data; and
generate a flight datum as a function of the measured aircraft data;
a computing device in the eVTOL aircraft and communicatively connected to the sensor, wherein the computing device is configured to:
receive the flight datum;
determine a current flight phase as a function of the flight datum, wherein the current flight phase includes a climb phase of the eVTOL aircraft which follows a lift-off phase of the eVTOL aircraft;
identify an input latency as a function of the flight datum and the current flight phase; and
select a lag frame as a function of the input latency, wherein the lag frame further comprises a lag threshold, wherein the lag frame associated with the climb phase is different than that associated with the lift-off phase, wherein the lag frame is set to a time value of the lag threshold if the selected lag frame reaches the time value of the lag threshold.
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