|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||G05D-001/06 G05D-001/08 B64C-013/16 B64D-031/06 B64D-043/02|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 6|
An aircraft stall protection system and method include calculating a first angle of attack and a second angle of attack based on aircraft configuration and environmental conditions, the first angle of attack being greater than the second angle of attack. The system and method limit the actual aircraft angle of attack to the first angle of attack for a predetermined period of time and thereafter the system and method limit the actual aircraft angle of attack to the second angle of attack. The system and method allow the aircraft operator or pilot to extra...
1. A method of controlling an aircraft at high angles of attack, the method comprising: measuring an actual angle of attack (α) for an aircraft;calculating a short term alpha (α1);calculating a long term alpha (α2);calculating an activation alpha (α3);determining if the actual angle of attack (α) is greater than α3;limiting the actual angle of attack (α) to the short term alpha (α1) by activating at least one of an elevator, a stabilizer, a thrust lever, and a spoiler;evaluating if a predetermined criteria has been met; andlimiting the actual angle of at...