|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/194; 244/221; 244/229; 244/099.4|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 11 인용 특허 : 71|
Embodiments of the invention relate to a flight control system for controlling an aircraft in flight having a backup control system integrated into an active control stick. The actuated control stick may include a processing unit that includes independent and separate hardware and/or software dedicated to the primary control system and the backup control system. For the primary control system, the processing unit may receive a sensed primary control stick signal and communicate with a primary processor, which may be configured to generate a primary contr...
1. A flight control system for controlling an aircraft in flight, the flight control system comprising: an actuated control stick comprising a primary sensor, a backup sensor, and a processing unit having at least one processor configured to generate a tactile signal for the actuated control stick;a set of primary electronics coupled to the primary sensor and located in the processing unit, the set of primary electronics being configured to receive a primary control stick signal from the primary sensor and to generate at least one primary control signal ...