[1]张博俊,王俊峰,李大鹏,等.简化弹道设计方法在运载火箭型号论证中的应用[J].弹道学报,2019,(03):12-17.[doi:10.12115/j.issn.1004-499X(2019)03-003]
 ZHANG Bojun,WANG Junfeng,LI Dapeng,et al.Application of Simplified Trajectory Design Algorithm inType Demonstration of Launch Vehicle[J].Journal Of Ballistics,2019,(03):12-17.[doi:10.12115/j.issn.1004-499X(2019)03-003]
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简化弹道设计方法在运载火箭型号论证中的应用()
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《弹道学报》[ISSN:1004-499X/CN:32-1343/TJ]

卷:
期数:
2019年03期
页码:
12-17
栏目:
出版日期:
2019-09-30

文章信息/Info

Title:
Application of Simplified Trajectory Design Algorithm inType Demonstration of Launch Vehicle
文章编号:
1004-499X(2019)03-0012-06
作者:
张博俊王俊峰李大鹏肖 清
北京宇航系统工程研究所,北京 100076
Author(s):
ZHANG BojunWANG JunfengLI DapengXIAO Qing
Beijing Institute of Aerospace System Engineering,Beijing 100076,China
关键词:
弹道优化 运载火箭 主动段
Keywords:
trajectory optimization launch vehicle active phase
分类号:
V412.1
DOI:
10.12115/j.issn.1004-499X(2019)03-003
摘要:
针对运载火箭构型不确定、目标轨道多、最优化设计工作量大的问题,提出了一种简化弹道设计方法。通过简化动力学方程及设计变量,将构型不确定且难以建模的非线性规划问题转变为适用于多种构型且方便寻优的简化弹道设计方法。对运载火箭执行不同的目标轨道任务进行了分析,将所有的任务按照有无滑行段进行了分类,提出了针对不同任务的弹道拼接方法。采用该简化弹道设计方法对CZ-3B和Falcon9 2种不同构型的火箭实际飞行曲线进行拟合,验证了简化弹道设计方法的正确性。
Abstract:
To solve the problems such as uncertain configuration,multiple target orbits requirements and huge workload of optimization design of launch vehicle,a simplified optimal trajectory design algorithm was proposed. By simplifying the dynamic equation and control variables,the non-linear programming problem which is difficult to be modeled due to uncertain configuration,was transformed into a simplified algorithm which is suitable for multiple launch configurations and convenient for optimization. Different orbit-mission requirements of launch vehicle were analyzed,and all the missions were classified according to whether there was a glide segment,and a trajectory splicing method for different missions was proposed. The actual flight curves of two kinds of launch vehicles CZ-3B and Falcon9 with different configurations were fitted by the simplified trajectory design algorithm. The simplified algorithm is correct.

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备注/Memo

备注/Memo:
收稿日期:2018-12-09
作者简介:张博俊(1986- ),男,工程师,硕士,研究方向为飞行力学,运载火箭弹道设计。E-mail:zhangbj_8611@126.com。
更新日期/Last Update: 2019-09-30