摘要
建立了飞机地面滑行动力响应分析模型,并基于ADAMS/Aircraft模块创建了飞机地面滑行仿真模型,仔细考虑了多种性能参数如轮胎刚度特性、轮胎与地面摩擦系数、跑道不平度等对起落架性能的影响。仿真结果表明,利用ADAMS/Aircraft进行起落架或全机仿真分析,可信度高,可节省大量的人力与时间,精度可靠,便于全机优化分析与改进设计。
It establishes a full-aircraft taxiing dynamic behavior analysis model,and based on ADAMS/Aircraft software establishes the full-aircraft taxiing simulation model. Influence of behavior parameters is carefully considered such as tire stiffness, friction coefficient with ground, runway profile. It proves highly reliable for ADAMS/Aircraft software to perform landing-gear or full- aircraft simulation analyses. It can save a lot of manpower and time,has reliable precision,suits optimization analysis and improving design of full-aircraft.
出处
《机械工程与自动化》
2007年第2期1-3,共3页
Mechanical Engineering & Automation
基金
安徽省高校青年教师自然科学科研资助项目(2004jq126)
关键词
全机
滑行
动力响应
仿真
full-aircraft
taxiing
dynamic behavior
simulation
