重复使用运载器末端能量管理段制导系统仿真  

Terminal Area Energy Management Guidance Scheme Simulation for Reusable Launch Vehicle

作　　者：孙春贞[1] 黄一敏[1] 

机构地区：[1]南京航空航天大学自动化学院,江苏南京210016

出　　处：《系统仿真学报》2007年第6期1260-1264,共5页Journal of System Simulation

摘　　要：为了对重复使用运载器末端能量管理段制导系统进行研究,根据末端能量管理段的制导策略,搭建了集成的、具有层次结构的制导系统仿真结构,将Matlab/Simulink、Stateflow和GUI有机结合起来,建立了易于维护和扩展的伪5自由度仿真环境。利用伪5自由度仿真环境对末端能量管理段的制导策略和制导规律进行了非线性仿真,结果表明了制导策略的合理性以及RLV伪5自由度非线性仿真环境的通用性和实用性。In order to research Terminal Area Energy Management （TAEM） guidance system for Reusable Launch Vehicle, the integrated and hierarchical architecture for guidance system was built. Integrating Matlab/Simulink and Stateflow and GUI, the pseudo-five-degree-of-freedom simulation environment was built, which is easy to maintenance and extent. The nonlinear simulation of TAEM guidance scheme and guidance law was completed. The results show that the guidance scheme is logical, and the simulation environment for Reusable Launch Vehicle is common and practical.

关 键 词：重复使用运载器 末端能量管理 制导 伪5自由度仿真 

分 类 号：V448[航空宇航科学与技术—飞行器设计] V249