摘要
总结了MA600飞机在适航取证过程中所做的APC/PIO研究与评估工作。根据APC/PIO产生的机理及类型,理论分析了MA600的APC/PIO易感性及可能发生的类型;选择适合于运输机的预测准则,对纵向和横向的APC/PIO易感性进行了评估和分析;制定了试飞大纲,由试飞员在全动飞行模拟器上完成了试飞任务,并对其APC/PIO趋势做出了评分和评语;最后,对试飞数据进行了分析,所得结果与理论分析结果、准则评估结果及试飞员评语一致,表明MA600飞机没有发生APC/PIO的趋势,满足适航条例对APC/PIO的要求。
The research and evaluation work of APC/PIO susceptibility for the MA600 aircraft is summarized.The APC/PIO susceptibility of the MA600 is analyzed theoretically from aspects of generation and causing.Proper evaluation criteria for a transport are chosen to evaluate and analyze the longitudinal and lateral APC/PIO susceptibility.Then the flight test program is established.Three flight test pilots rated and evaluated the APC/PIO tendencies of the MA600 aircraft after finishing these flight test tasks on a full-flight simulator.The analysis of the flight test data shows the evaluation accords with the theoretical results,the criteria evaluation results and the flight test pilot＇s comments,which indicates that the MA600 aircraft does not have APC/PIO tendencies and satisfies the requirements of the airworthiness criteria.
出处
《飞行力学》
CSCD
北大核心
2010年第6期6-10,15,共6页
Flight Dynamics
关键词
民用飞机
适航取证
APC/PIO易感性
准则评估
试飞大纲
civil aircraft
airworthiness certification
APC/PIO susceptibility
criterion evaluation
flight test program
