论文部分内容阅读
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 - track” principle of the slip angle calibration test technology and three different side slip angle measurement methods (front strut method, fuselage weather vane method and static pressure difference method) to study and summarize Civil aircraft side slip angle calibration research project research results. The side slip angle is an important input condition for many test subjects (lateral stability, yaw maneuver test, etc.). The Administrator requires the calibration of the side slip angle and must be completed during the aircraft design phase. Therefore, the author organized demonstration of side-slip angle calibration related to the requirement of front strut installation in the preliminary preparation stage of the project, and the scientific approach of project management plays an important role in advancing the side-slip angle calibration of the other aircraft.