摘要
以工程应用为出发点,提出了试验机技术状态确定的依据、单次无维修待命时间验证成败判据、特殊气象条件下试验数据处理方法、无维修待命时间验证评估模型。在此基础上,以某型歼击机为例给出了试飞阶段无维修待命时间验证方案设计方法。该方法工程应用性强,可作为试飞阶段外场开展无维修待命时间验证的依据。
Focusing on engineering application,the determination method of configuration requirements,failure criteria of test,data processing method under extreme environment and evaluation model for maintenance-free alert time were proposed. Then,verification scheme design method of maintenance-free alert time for fighter plane during flight test was given as an example based on this theory. The result shows strong engineering applicability and the verification of maintenance-free alert time during flight test can be conducted based on it.
出处
《飞行力学》
CSCD
北大核心
2016年第2期81-85,共5页
Flight Dynamics
基金
"十二五"国防技术基础科研项目(Z052013B004)
关键词
无维修待命时间
试验机
技术状态
试验方案设计
maintenance-free alert time
testing aircraft
configuration
test scheme design
