发明名称 |
Complemented roll attitude flight control system |
摘要 |
A system and technique is disclosed which provides a complemented roll attitude signal for use in the control system of an aircraft. The complemented roll attitude is produced by combining a yaw rate and true airspeed signal with a conventional roll attitude signal to produce a complemented signal which may be combined with a roll command signal to produce a roll steering signal for controlling aircraft response under non-zero roll attitude conditions of aircraft flight. The complemented roll attitude signal provides improved response to aircraft roll commands under non-zero roll attitude conditions, particularly in helicopter systems.
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申请公布号 |
US4553210(A) |
申请公布日期 |
1985.11.12 |
申请号 |
US19820408962 |
申请日期 |
1982.08.17 |
申请人 |
ROCKWELL INTERNATIONAL CORPORATION |
发明人 |
CENTALA, JOHN P. |
分类号 |
G05D1/08;(IPC1-7):G06F15/30 |
主分类号 |
G05D1/08 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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