ACCELERATION SMOOTHING HOLDING OVERALL KINETIC ENERGY CONTROL
摘要
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.
申请公布号
EP2940546(A3)
申请公布日期
2016.03.23
申请号
EP20150165699
申请日期
2015.04.29
申请人
SIKORSKY AIRCRAFT CORPORATION
发明人
AGNIHOTRI, ASHOK;WEINER, STEPHEN D.;SAHASRABUDHE, VINEET