发明名称 |
Method and apparatus for aircraft pitch and thrust axes control |
摘要 |
An aircraft automatic of semiautomatic vertical path control system which coordinates operation of pitch and engine thrust control systems to transfer speed control from one system to the other depending on a requirement to climb, descend, or maintain altitude as determined by the polarity and magnitude of the difference between a selectable desired altitude and current actual altitude.
|
申请公布号 |
US4471439(A) |
申请公布日期 |
1984.09.11 |
申请号 |
US19830546255 |
申请日期 |
1983.10.28 |
申请人 |
THE BOEING COMPANY |
发明人 |
ROBBINS, RICHARD E.;SIMPSON, ROBERT D. |
分类号 |
G05D1/06;(IPC1-7):G05D1/08 |
主分类号 |
G05D1/06 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|