| Citation: | ZHOU Jingliang, CHEN Xiong, CHAI Jinbao. Control algorithms for adjustable flow gas generator of ducted ramjet[J]. Journal of Aerospace Power, 2020, 35(5): 1109-1120. doi: 10.13224/j.cnki.jasp.2020.05.022
|
| [1] |
FRY R S.A century of ramjet propulsion technology evolution［J］.Journal of Propulsion and Power,2004,20(1):27-58.
|
| [2] |
曹军伟,何国强,王希亮,等.空空导弹固体火箭冲压发动机设计参数优化［J］.航空动力学报,2015,30(8):2018-2024. CAO Junwei,HE Guoqiang,WANG Xiliang,et al.Parameter optimization design of air-ducted rocket for airborne missile［J］.Journal of Aerospace Power,2015,30(8):2018-2024.(in Chinese)
|
| [3] |
TOKUNAGA H,KOORI K,IKEGAMI Y,et al.Development of wide-range dupersonic intake for variable flow ducted rocket engine［R］.AIAA-2009-5223,2009.
|
| [4] |
何勇攀,陈玉春,于守志,等.固体火箭冲压发动机燃气发生器动态特性影响分析［J］.航空动力学报,2017,32(1):228-232. HE Yongpan,CHEN Yuchun,YU Shouzhi,et al.Analysis on influence of dynamic characteristics of gas generator in solid propellant ducted rockets［J］.Journal of Aerospace Power,2017,32(1):228-232.(in Chinese)
|
| [5] |
周建军.固体火箭冲压发动机燃气流量调节技术与实验研究［J］.弹箭与制导学报,2005,25(4):558-560. ZHOU Jianjun.Gas flow control technique of rocket ram-jet［J］.Journal of Projectiles,Rockets,Missiles and Guid-ance,2005,25(4):558-560.(in Chinese)
|
| [6] |
MAYER A E H J,HALSWIJK W H C,KOMDUUR H J.A modular ducted rocket missile model for threat and performance assessment［R］.AIAA 2005-6013,2005.
|
| [7] |
BESSER H L,WEINREICH H L,KURTH G.Fit for mission-design tailoring aspects of throttleable ducted rocket propulsion systems［R］.AIAA 2008-5262,2008.
|
| [8] |
李博,于新宇,谢侃,等.固体火箭发动机流体喉部推力矢量特性［J］.航空动力学报,2016,31(12):2996-3003. LI Bo,YU Xinyu,XIE Kan,et al.Thrust vectoring fea-tures about fluidic throat for solid rocket motor［J］.Journal of Aerospace Power,2016,31(12):2996-3003.(in Chinese)
|
| [9] |
何坤.锥阀式燃气流量调节系统设计与实验研究［D］.南京:南京理工大学,2017. HE Kun.Design and experimental study of cone valve type gas flow regulating system［D］.Nanjing:Nanjing University of Science and Technology,2017.(in Chinese)
|
| [10] |
何坤,陈 雄,郑 健,等.模糊PI控制算法在燃气发生器上的应用［J］.推进技术,2017,38(8):1878-1884. HE Kun,CHEN Xiong,ZHENG Jian,et al.Fuzzy PI control algorithm for gas generator［J］.Journal of Propulsion Technology,2017,38(8):1878-1884.(in Chinese)
|
| [11] |
聂聆聪,刘志明,刘源祥.流量可调燃气发生器压力闭环模糊控制算法［J］.推进技术,2013,34(4):551-556. NIE Lingcong,LIU Zhiming,LIU Yuanxiang.Pressure close loop fuzzy control method of a flow adjustable gas generator［J］.Journal of Propulsion Technology,2013,34(4):551-556.(in Chinese)
|
| [12] |
刘源翔,姚晓先,聂聆聪,等.一种流量可调燃气发生器压强控制算法的研究［J］.固体火箭技术,2014,37(1):43-47. LIU Yuanxiang,YAO Xiaoxian,NIE Lingcong,et al.Research on pressure control algorithm of flow adjustable gas generatol［J］.Journal of Solid Rocket Technology,2014,37(1):43-47.(in Chinese)
|
| [13] |
赵泽敏.固体火箭冲压发动机燃气流量调节控制系统研究［D］.南京:南京理工大学,2014. ZHAO Zemin.Research on gas flow control system of solid rocket ramjet［D］.Nanjing:Nanjing University of Science and Technology,2014.(in Chinese)
|
| [14] |
韩京清.自抗扰控制技术:估计补偿不确定因素的控制技术［M］.北京:国防工业出版社,2008.
|
| [15] |
朱斌.自抗扰控制入门［M］.北京:北京航空航天大学出版社,2017.
|
| [16] |
武晓松,陈军,王栋.固体火箭发动机原理［M］.北京:兵器工业出版社,2010:236-239.
|
| [17] |
马立坤.燃气流量可调固体火箭冲压发动机动态响应过程研究［D］.长沙:国防科技大学,2011. MA Likun.Investigation of the response process of variable flow ducted rocket［D］.Changsha:National University of Defense Technology,2011.(in Chinese)
|
| [18] |
钱秋朦,但志宏,张松,等.航空发动机过渡态试验进气压力线性自抗扰控制方法［J］.航空动力学报,2019,34(10):2271-2279. QIAN Qiumeng,DAN Zhihong,ZHANG Song,et al.Linear active disturbance rejection control method for intake pressure control in aero-engine transient test［J］.Journal of Aerospace Power,2019,34(10):2271-2279.(in Chinese)
|
| [19] |
ALONGE F,CIRRINCIONE M,D’IPPOLITO F,et al.Robust active disturbance rejection control of induction motor systems based on additional sliding-mode component［J］.IEEE Transactions on Industrial Electronics,2017,64(7):5608-5621.
|
| [20] |
TAN W,FU C.Linear active disturbance-rejection control:analysis and turning via IMC［J］.IEEE Transactions on Industrial Electronics,2016,63(4):2350-2359.
|
| [21] |
张海波,孙健国,孙立国.一种涡轴发动机转速抗扰控制器设计及应用［J］.航空动力学报,2010,25(4):943-950. ZHANG Haibo,SUN Jianguo,SUO Liguo.Design and application of a disturbance rejection rotor speed control method for turbo-shaft engines［J］.Journal of Aerospace Power,2010,25(4):943-950.(in Chinese)
|
| [22] |
徐秋坪,常思江,王中原.自适应网格跟踪微分器设计［J］系统工程与电子技术,2018,40(6):1212-1220. XU Qiuping,CHANG Sijiang,WANG Zhongyuan.Design of adaptive mesh tracking differentiator［J］.Systems Engineering and Electronics,2018,40(6):1212-1220.(in Chinese)
|
| [23] |
WEI Y H,HU Y S,SONG L,et al.Tracking differentiator based fractional order model reference adaptive control the 1<α<2 case［C］∥Proceedings of the 53rd IEEE Annual Conference on Design and Control.Los Angeles,US:IEEE,2014:6902-6907.
|
| [24] |
WEI J X,GAO Z.Design and analysis on fractional-order tracking differentiator［C］∥Proceedings of the 27th IEEE Chinese Control and Decision Conference.Qingdao:IEEE,2015:6128-6132.
|
| [25] |
王建华,刘鲁华,王鹏,等.带三维落角约束的寻的导弹制导与姿控系统设计［J］.国防科技大学学报,2017,39(1):30-39. WANG Jianhua,LIU Luhua,WANG Peng,et al.Guidance and control system design for homing missiles with three dimensional impact angle constraints［J］.Journal of National University of Defense Technology,2017,39(1):30-39.(in Chinese)
|
| [26] |
GUO B Z,ZHAO Z L.On the convergence of extended state observer for nonlinear systems with experimentation［J］.System and Control Letters,2011,60(6):420-430.
|
| [27] |
孙佃升,章跃进.线性扩张状态观测器的改进及观测精度分析［J］.国防科技大学学报,2017,39(6):111-117. SUN Diansheng,ZHANG Yuejin.Improvement and observation accuracy analysis of linear extended state observer［J］.Journal of National University of Defense Technology,2017,39(6):111-117.(in Chinese)
|
| [28] |
GAO Z Q.Scaling and bandwidth-parameterization based controller tuning［C］∥Proceedings of the 2003 American Control Conference.Denver,US:IEEE,2003:4989-4996.
|
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