摘要
对基于"航向-航迹"原理的侧滑角校准试飞技术以及三种不同的侧滑角测量方法(前支杆法,机身风标法和静压差值法)进行研究,总结民用飞机侧滑角校准研究项目的研究成果。侧滑角是许多试飞科目(横航向静稳定性、偏航机动试飞等)开展的重要输入条件,局方要求必须进行侧滑角校准,且在飞机设计阶段就要完成。因此,作者在项目前期准备阶段组织了侧滑角校准涉及到前支杆加装需求的论证工作,运用项目管理的科学办法对侧滑角校准他机验证试飞技术攻关项目的推进具有重要作用。
Based on the course--the principles of track slip angle calibration technology and test three different slip angle measuring method （method strut front fuselage wind standard method and static differential pressure method）, the results were summed up for the civil aircraft slip angle calibration. The slip angle is an important entering condition for many test subjects （ lateral and directional static stability, yaw maneuver test, etc. ） The Bureau requested that the sideslip angle calibration must be done , and completed during the aircraft design phase. So the author organized strut installation requirements related to the sideslip angle adjustment related to feasi -bility studies before the project preparation stage. The scientific approach in this paper has played an important role for other aircraft verification test technology of side slip angle calibration.
出处
《民用飞机设计与研究》
2016年第4期80-84,共5页
Civil Aircraft Design & Research
关键词
侧滑角校准
他机验证
项目管理
sideslip angle calibration
other aircraft verification
project management
