摘要
介绍了飞行器控制导引一体化设计方法的研究现状及发展背景.提出了导弹控制导引一体化设计的性能要求.最后指出了当前飞行器控制导引一体化设计存在的主要问题和值得深入研究的方向.
The research state and developing background of integrated design method for air vehicle’s guidance and control are introduced. The desired performance of integrated design for missile’s guidance and control is brought forward. Finally, after the main problems at present in the integrated design of air vehicle’s guidance and control are given, the direction of further research on the integrated design of air vehicle’s guidance and control is pointed out.
出处
《海军航空工程学院学报》
2006年第2期227-230,共4页
Journal of Naval Aeronautical and Astronautical University
关键词
飞行器
控制
导引
一体化
air vehicle
control
guidance
integration
