A method and system for controlling maneuverability of an aircraft includes receiving one or more signals indicative of commanded peak rotary acceleration at a first timeperiod; determining a signal indicative of an actual peak rotary acceleration for the first timeperiod in response to the receiving of the one or more signals for commanded pilot acceleration; and determining signals indicative of actual rotary acceleration for a second timeperiod.
ACCELERATION SMOOTHING HOLDING OVERALL KINETIC ENERGY CONTROL
2015-11-05
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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