|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 46 인용 특허 : 15|
A flight control module with integrated actuator spoiler control electronics, where the flight control functions have been integrated into the integrated modular avionics through the use of a flight control module ("FCM"), the FCM being configured to contain spoiler actuator control electronics ("ACE"). The spoiler ACE is used to control the roll functions of the spoiler. The spoiler ACE is configured to be separate from the FCM, even though it is located within the same modules and receives its power independent of the power supply for the FCM. In the e...
1. A module for insertion into an integrated modular avionics unit for use in an airplane comprising: a flight control computer; and actuator control electronics coupled to a spoiler; wherein said module is inserted into the integrated modular avionics unit and said flight control computer augments control of the airplane, and wherein said actuator control electronics is configured to operate said spoiler in the event of a failure of said flight control computer to provide backup roll control of said airplane. 2. The module of claim 1 wherein, ...