摘要
提出了一种进行单级和多级火箭飞行方案设计的一般方法。这是一种基于微积分变分原理的工程方法。其目的是根据给定导弹的攻角方案设计其俯仰角方案。最大攻角的优化根据给定的初始设计值采用正交法进行。该方法可以快速地进行多级火箭的飞行方案设计。
A generalized approach to flight program design for single and multi-stage rockets are presented. This approach uses an engineering method based on the principle of calculus variation. Its object is to design the pitch program fora missile by giving attack angle program. The optimization of maximum attack angle is evaluated according to the given initial design parameters by using the orthogonal method. This approach is efficient for flight program design of multi-stage rockets .
出处
《航空学报》
EI
CAS
CSCD
北大核心
2005年第1期50-53,共4页
Acta Aeronautica et Astronautica Sinica
关键词
弹道导弹
飞行方案
优化
ballistic missile
flight program
optimization
