|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/83D ; 244/178 ; 244/195 ; 244/196|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 37 인용 특허 : 1|
The present steering mechanism, especially for an aircraft includes a manually operable steering member and an automatic steering system. A difference signal formed from a pilot input and trim signal and from a gyro feedback signal is supplied to a force control and damping circuit twice, once directly and once through an authority limit circuit. The output of the authority limit circuit is also supplied to the motors forming part of the automatic steering system. The force control and damping circuit also receives further input signal or signals represe...
The steering mechanism with an active force feedback, especially for an aircraft, comprising a manual steering means, automatic steering means, signal providing means including pitch position sensor means (10′) operatively connected to said manual steering means to provide a pilot trim control signal, pitch rate gyro means (13) providing a gyro feedback signal, signal processing means including differential amplifier means (12) operatively connected to said pitch position sensor means and to said pitch rate gyro means for providing a difference output si...