|Table of Contents|

Analysis on control torque reconstruction of launch vehicle after thrust drop(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2023年01期
Page:
21-28
Research Field:
目次
Publishing date:

Info

Title:
Analysis on control torque reconstruction of launch vehicle after thrust drop
Author(s):
CHEN Yuqiang CUI Mengyu XIE Changlin YANG Shuming
(College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China)
Keywords:
thrust drop control torque control allocation modified simplex method attitude reconstruction
PACS:
V249
DOI:
-
Abstract:
Aiming at the problem of sudden thrust drop for active service strap-on rocket during flight, a control allocation method based on improved simplex method is proposed.Based on the idea that the control torque of the rocket is equal before and after the failure, the redistribution problem of rocket engine swing angle after thrust drop is transformed into a linear distribution problem under the constraint of objective function, which is effectively solved by the improved simplex method.The results show that the yaw angle can quickly return to the equilibrium state after the shutdown failure, and the roll angle can also quickly return to stability after a small buffeting.This algorithm can effectively improve the weakening of the control ability after the sudden thrust drop of the rocket engine, and maintain the stability of the rocket attitude after the failure.The research content has theoretical significance and engineering application value for the attitude reconstruction of launch vehicle.

References:

[1] 张鑫伟,付郁.2020年全球航天发射统计分析[J].国际太空,2021(2):18-23.
[2] 夏鲁瑞.液体火箭发动机涡轮泵健康监控关键技术及系统研究[D].长沙:国防科学技术大学,2010.
[3] 龙乐豪.液体弹道导弹与运载火箭系列:总体设计[M].北京:中国宇航出版社,2001.
[4] 曲晶,张绿云.国外火箭发射及故障情况统计分析[J].中国航天,2016(2):13-18.
[5] 马军强,杨思锋,戴芳立.基于RVM的液体火箭发动机试验台故障预测方法[J].火箭推进,2015,41(3):80-86.
MA J Q,YANG S F,DAI F L.RVM-based fault prediction method for liquid rocket engine test stand[J].Journal of Rocket Propulsion,2015,41(3):80-86.
[6] 张伟星,李建民,侯文,等.BP神经网络用于火箭增压输送系统故障检测[J].火箭推进,2021,47(5):85-91.
ZHANG W X,LI J M,HOU W,et al.BP neural network applied in fault detection of rocket pressurized delivery system[J].Journal of Rocket Propulsion,2021,47(5):85-91.
[7] 宋征宇.从准确、精确到精益求精:载人航天推动运载火箭制导方法的发展[J].航天控制,2013,31(1):4-10.
[8] CALISE A J,LEE S,SHARMA M.Development of a reconfigurable flight control law for tailless aircraft[J].Journal of Guidance,Control,and Dynamics,2001,24(5):896-902.
[9] 吴蕾.考虑发动机推力损失的运载火箭容错控制[D].大连:大连理工大学,2019.
[10] BUFFINGTON J M,ENNS D F.Lyapunov stability analysis of daisy chain control allocation[J].Journal of Guidance,Control,and Dynamics,1996,19(6):1226-1230.
[11] 胥彪,周荻.基于反步法及控制分配的导弹直接侧向力/气动力复合控制[J].系统工程与电子技术,2014,36(3):527-531.
[12] DURHAM W C.Constrained control allocation:Three-moment problem[J].Journal of Guidance,Control,and Dynamics,1994,17(2):330-336.
[13] DURHAM W C.Attainable moments for the constrained control allocation problem[J].Journal of Guidance,Control,and Dynamics,1994,17(6):1371-1373.
[14] 杨凌宇,高金源,申功璋.飞行控制中的一种新型最优控制分配方法[J].北京航空航天大学学报,2007,33(5):572-576.
[15] 程堂明,陈宇.适应伺服机构卡死故障的控制指令重分配技术研究[J].导弹与航天运载技术,2017(1):51-55.
[16] 冯昊,李新明,潘豪.大推力运载火箭控制系统控制力重构技术研究[J].载人航天,2012,18(6):75-79.
[17] 贾沛然,陈克俊,何力.远程火箭弹道学[M].长沙:国防科技大学出版社,1993.
[18] 王志祥.推力下降故障下运载火箭轨迹在线生成与姿控系统重构[D].长沙:国防科学技术大学,2016.
[19] ARSHAM H.An algorithm for simplex tableau reduction:The push-to-pull solution strategy[J].Applied Mathematics and Computation,2003,137(2/3):525-547.
[20] 敖特根.单纯形法的产生与发展探析[J].西北大学学报(自然科学版),2012,42(5):861-864.

Memo

Memo:
-
Last Update: 1900-01-01