A Guidance Method for Small Solid-Rocket Launch Vehicles

被引：0
|
作者：
Lv, Rui [1 ]
Song, Zhiguo [1 ]
Li, Pu [1 ,2 ]
Jiang, Chunwang [1 ]
Ge, Yunpeng [1 ]
机构：
[1] China Acad Launch Vehicle Technol, Beijing 100076, Peoples R China
[2] Natl Univ Def Technol, Changsha 410073, Peoples R China
来源：
2018 IEEE CSAA GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC) | 2018年
关键词：
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
This paper presents a guidance method for solid-rocket launch vehicles. A three-stage launch vehicle, as illustration, the guidance algorithm is designed for the second stage and the third stage. For the second stage, the guidance algorithm guides the vehicle to a transfer orbit, and high precision orbit injection is implemented by the guidance algorithm for the third stage. Numerical simulation results show that the proposed guidance method can achieve an adequate precision with the burnout shutdown.
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页数：3
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