Dynamically Modeling and Analysis of Thrust Measurement System for Solid Ramjet
Received date: 2015-11-08
Online published: 2025-05-30
谢海刚 , 李纲 . 固冲发动机推力测量系统动态建模与分析[J]. 弹箭与制导学报, 2016 , 36(3) : 73 -77,81 . DOI: 10.15892/j.cnki.djzdxb.2016.03.020
For ignition thrust measurement distortion of solid ramjet in ground test, a dynamic model for thrust measurement system was built.The responses at different excitation signals were obtained by designing and implementing identification test which based on ARMAX model.According to the test results, structure and order were identified and the dynamic model for thrust measurement system was built.Veracity and effectiveness of model were verified by fitting rate analysis and residual whiteness estimation.Time-frequency domain analysis results show that the dynamic model could be used to reflect actual dynamic characteristics of thrust measurement system, laying a foundation for improvement of dynamic characteristics, adding thrust compensation and real signals resume.
Key words: solid ramjet; thrust measurement; dynamically modeling
| [1] | DEAN D S, 张峻城. 火箭发动机推力瞬变的测量[J]. 固体火箭技术, 1982 (2): 106-115. |
| [2] | 欧阳华兵 固体火箭发动机瞬态推力测量[D]. 杭州: 浙江工业大学, 2005: 11-14. |
| [3] | SASOH Akihiro, ARAKAWA Yoshihira. A high-resolution thrust stand for ground tests of low-thrust space propulsion devices[J]. Rev.Sci.Instrum, 1993, 64(3): 719-723. |
| [4] | 李俊华, 张平. 动态推力频域恢复技术[J]. 固体火箭技术, 1996, 19(1): 69-74. |
| [5] | 赵自文. 动态推力校准系统设计[J]. 自动化仪表, 2007, 28(增利): 228-230. |
| [6] | 侯媛彬, 汪海, 王立琦,等. 系统辨识及其 Matlab 仿真[M]. 北京: 科学出版社, 2004: 81-88. |
| [7] | LJUNG Lennart. System Identification Toolbox:User's Guide[M]. MathWorksInv, 1995: 17-24. |
/
| 〈 |
|
〉 |