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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
---|---|
국제특허분류(IPC7판) |
|
출원번호 | US-0306336 (1981-09-25) |
발명자 / 주소 |
|
출원인 / 주소 |
|
인용정보 | 피인용 횟수 : 6 인용 특허 : 5 |
An aircraft speed control system wherein the commanded lift floor (minimum lift) is increased in accordance with an anticipated decrease in headwind between headwind during final landing approach and that anticipated at touchdown. The system includes means for generating a signal which is a function
In an aircraft speed control system including means for providing a first signal which is a function of airspeed error constituting the difference between actual airspeed and a pilot selected airspeed, means for providing a second signal which is a function of lift error (alpha error) constituting t
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