摘要
介绍了某型歼击机全任务飞行模拟器的系统结构,针对该型歼击机的特点,详细讨论了在其飞行系统的建模与验模中应该考虑的各种因素、应遵循的原则及其实现方法等,并通过实例对其进行了验证。结果表明,方法是合理的。
The system structure of a fullmission fighter simulator is introduced in this paper.In accordance with the characteristic of this fighter,various factors, principles of design and its realizing method in the modeling and VV&A for its flying system are discussed in detail.All of these are tested and verified by a example,and the result shows that the method is reasonable.
出处
《飞行力学》
CSCD
2003年第3期59-62,共4页
Flight Dynamics
