| 直升机贴地飞行时人—机响应特性研究 |
| |
| 引用本文： | 杨松山.直升机贴地飞行时人—机响应特性研究[J].飞行力学,1992(2). |
| |
| 作者姓名： | 杨松山 |
| |
| 作者单位： | 飞行试验研究院 |
| |
| 摘 要： | 本文分析和研究了驾驶员工作负荷、操纵功效和阻尼等对贴地飞行时直升机飞行品质的影响,导出了简化的驾驶员增益和驾驶员评定等级的工程计算公式,并与飞行试验数据进行了比较.结果表明,本文的方法可用于各种直升机的飞行试验和设计估算.
|
| 关 键 词： | 直升机 驾驶员增益 驾驶员评定等级 飞行品质 |
CHARACTERS OF HUMAN-HELICOPTER CLOSED-LOOP RESPOND FOR NOE FLIGHT |
| |
| Yang Songshan.CHARACTERS OF HUMAN-HELICOPTER CLOSED-LOOP RESPOND FOR NOE FLIGHT[J].Flight Dynamics,1992(2). |
| |
| Authors: | Yang Songshan |
| |
| Institution: | Chinese Flight Test Establishment |
| |
| Abstract: | This paper analyses and studies effects of pilot stress, control power and damping on flight qualities of helicopter, the simplify engineering computation formula for pilot gain and pilot assessments have been direved, and the results compare with flight test data. The results show that the technique in this paper is suitable to any helicopter flight test and design estimate. |
| |
| Keywords: | Helicopter Pilot gain Pilot assessments class Flight qualities |
| 本文献已被 CNKI 等数据库收录！ |
