INTEGRATED FLIGHT/PROPULSION CONTROL FOR HELICOPTERS

被引：2
|
作者：
ROCK, SM
NEIGHBORS, K
机构：
来源：
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY | 1994年 / 39卷 / 03期
关键词：
D O I：
10.4050/JAHS.39.34
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Presented is a procedure for improving the communication of requirements and specifications in the early design phases of an integrated helicopter/engine control system. The procedure is based on establishing a bound on a transfer matrix, Delta(Omega U)(s), that relates blade cyclic and collective inputs to rotor speed variations. This bound becomes a new specification for the propulsion control system designer that embodies the mission-level performance goals of the helicopter. An example application of the procedure is provided for a Blackhawk/T700 system undergoing vertical accelerations from hover.
引用
收藏
页码：34 / 42
页数：9
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