摘要
在介绍迭代制导原理的基础上,论述了工程应用中的可靠性设计方法,并以载人运载火箭为模型进行数学仿真,对迭代制导的可靠性、适应性、精度以及应用中的问题等进行了探讨。仿真表明,迭代制导方法具有很强的弹道适应性和良好的制导精度。
This paper introduces the theory of iterative guidance, illustrates the reliability design methods in the engineering application, discusses more in detail about the reliability, adaptability, precision and the problems in practical applications according to the mathematical simulation of the launch vehicle, and concludes that the simulation validates an extremely strong trajectory adaptability and a satisfactory guidance precision of the herative Guidance method.
出处
《载人航天》
CSCD
2009年第1期9-14,共6页
Manned Spaceflight
关键词
运载火箭
迭代制导
可靠性设计
数学仿真
Launch Vehicle
herative Guidance
Reliability Design
Mathematical Simulation
