运载火箭自适应增广控制参数设计及稳定性裕度分析

doi:10.12305/j.issn.1001-506X.2024.01.31

Abstract

Abstract:

In view of the design requirements of robust attitude control system in the ascent phase of launch vehicle, a parameter design method of adaptive augmenting controller (AAC) and a stability margin analysis method are proposed. Firstly, the small disturbance linearization equations and transfer functions are established for the conventional launch vehicle, and the proportional-derivative (PD) controller and the correction network are designed based on characteristic point parameters. Then, an AAC design is carried out, and the specific design method and criterion of the adjustment parameters are given. To further evaluate the stability of the whole control system after the addition of AAC, the sine response model of AAC is derived based on the sine analysis method. Therefore, the stability of the system can be evaluated. Finally, the actual six degree of freedom (6-DOF) simulation analysis is completed under various disturbance conditions, which proves the effectiveness of AAC. Moreover, the amplitude margin and phase margin of the AAC+PD control system are obtained. The simulation results show that the method can reflect the stability of the actual system, and it has certain engineering guiding significance.

Key words: launch vehicle, adaptive augmenting control, parameter design rule, stability analysis

CLC Number:

V475

Liang ZHANG, Si LIU, Kangwei ZHAO, Cunming HU. Parameters design and stability margin analysis of adaptive augmenting control for launch vehicle[J]. Systems Engineering and Electronics, 2023, 46(1): 271-279.

Figures/Tables 9

Fig.1

Fig.2

Fig.3

Fig.4

Fig.5

Fig.6

Fig.7

Fig.8

Fig.9

References 36

1	JEB S O, TANNEN V Z. Robust, practical adaptive control for launch vehicles[C]//Proc. of the AIAA Guidance, Navigation, and Control Conference, 2012.
2	HANSON J, CHARLES H. Learning about Ares I from Monte Carlo simulation[C]//Proc. of the AIAA Guidance, Navigation, and Control Conference, 2008.
3	BRIAN D L, RATNESHWAR J. Launch vehicle ascent flight control augmentation via a hybrid adaptive controller[C]//Proc. of the AIAA Guidance, Navigation and Control Conference and Exhibit, 2008.
4	TANNEN S V, ERIC T G, JOHN H W. In-flight suppression of an unstable F/A-18 structural mode using the space launch system adaptive augmenting control system[C]//Proc. of the AIAA Guidance, Navigation, and Control Conference, 2015.
5	TANNEN S V, ERIC T G, JOHN H W. Adaptive augmenting control flight characterization experiment on AN F/A-18[C]//Proc. of the American Astronautical Society Guidance, Navigation, and Control Conference, 2014.
6	CORNELIUS J D , TANNEN S V , CURTIS E H , et al. Flight testing of the space launch system (SLS) adaptive augmenting control (AAC) algorithm on an F/A-18[J]. USA: NASA, 2014,
7	MILLER C J. Nonlinear dynamic inversion baseline control law: flight-test results for the full-scale advanced systems testbed F/A-18 airplane[C]//Proc. of the AIAA Guidance, Navigation, and Control Conference, 2011.
8	CURT H, CHRIS M, JOHN H W. Launch vehicle manual steering with adaptive augmenting control: in-flight evaluations of adverse interactions using a piloted aircraft[C]//Proc. of the AIAA Guidance, Navigation, and Control Conference, 2015.
9	LUKE M, JING P, PAUL R. Demonstration of the space launch system augmenting adaptive control algorithm on a quad-rotor[C]//Proc. of the AIAA Guidance, Navigation, and Control Conference, 2018.
10	DIEGO N T, ANDRES M, SAMIR B, et al. Joint robust structured design of VEGA launcher's rigid-body controller and bending filter[C]//Proc. of the 69th International Astronautical Congress, 2018.
11	DIEGO N T, ANDRES M, SAMIR B, et al. Robust-control-based design and comparison of an adaptive controller for the VEGA launcher[C]//Proc. of the AIAA Scitech Forum, 2019.
12	JING P, PAUL R. Demonstration of the space launch system augmenting adaptive control algorithm on pole-cart platform[C]// Proc. of the AIAA Guidance, Navigation, and Control Conference, 2018.
13	BRINDA V , ARJUN N , SMRITHI U , et al. Classical adaptive augmentation control for a typical second generation launch vehicle[J]. IFAC PapersOnLine, 2016, 49 (1): 670- 675. doi: 10.1016/j.ifacol.2016.03.133
14	TANNEN V, ZHU J J, ADAMI T. Stability assessment and tuning of an adaptively augmented classical controller for launch vehicle flight control[C]//Proc. of the American Astronautical Society Guidance, Navigation, and Control Conference, 2014.
15	SUSAN A F, MARK J B, ALAN D W. Augmented adaptive control of a wind turbine in the presence of structural modes[C]// Proc. of the American Control Conference, 2010.
16	JOHN H W, JEB S O, TANNEN S V. Space launch system implementation of adaptive augmenting control[C]//Proc. of the American Astronautical Society Guidance, Navigation, and Control Conference, 2014.
17	JEB S O, JOHN H W, TANNEN S V, et al. Space launch system ascent flight control design[C]//Proc. of the AAS Guidance, Navigation, and Control Conference, 2014.
18	TROTTA D , ZAVOLI A , MATTEIS G D , et al. Tracking filter integration in the adaptive augmenting controller of a launch vehicle[J]. Journal of Guidance, Control, and Dynamics, 2021, 44 (12): 2327- 2336. doi: 10.2514/1.G006007
19	JEB S O. Modeling and test of space launch system core stage thrust vector control[C]//Proc. of the Aerospace Control and Guidance Systems Committee Meeting, 2016.
20	陈志勇. 柔性关节空间双臂机器人奇异摄动增广鲁棒自适应PD复合控制[J]. 振动与冲击, 2015, 34 (16): 79- 84.
	CHEN Z Y . Singular perturbation augmented robust adaptive PD composite control for flexible-joint dual-arm space robot[J]. Journal of Vibration and Shock, 2015, 34 (16): 79- 84.
21	陈力, 刘延柱. 参数不确定空间机械臂系统的增广自适应控制[J]. 航空学报, 2000, 21 (2): 150- 154. doi: 10.3321/j.issn:1000-6893.2000.02.012
	CHEN L , LIU Y Z . Adaptive control of space-based manipulator with uncertain parameters[J]. Acta Aeronautica et Astronautica Sinca, 2000, 21 (2): 150- 154. doi: 10.3321/j.issn:1000-6893.2000.02.012
22	洪昭斌, 陈力. 双臂空间机器人相对载体运动的增广自适应控制方法[J]. 力学季刊, 2007, 28 (3): 375- 381. doi: 10.3969/j.issn.0254-0053.2007.03.004
	HONG Z B , CHEN L . Adaptive control of spacecraft referenced end points motion of free floating dual arm space robot system[J]. Chinese Quarterly of Mechanics, 2007, 28 (3): 375- 381. doi: 10.3969/j.issn.0254-0053.2007.03.004
23	高军礼, 邓则名, 李芳. 可调增益的模型参考自适应控制及其仿真[J]. 信阳师范学院学报(自然科学版), 2001, 14 (3): 341- 343. doi: 10.3969/j.issn.1003-0972.2001.03.026
	GAO J L , DENG Z M , LI F . Gain-adjustable model reference adaptive control and simulation[J]. Journal of Xinyang Teachers College (Natural Science Edition), 2001, 14 (3): 341- 343. doi: 10.3969/j.issn.1003-0972.2001.03.026
24	肖冰, 胡庆雷, 马广富. 挠性卫星姿态跟踪自适应L2增益控制[J]. 控制理论与应用, 2011, 28 (1): 101- 107.
	XIAO B , HU Q L , MA G F . Adaptive L2-gain controller for flexible spacecraft attitude tracking[J]. Control Theory & Applications, 2011, 28 (1): 101- 107.
25	张建明, 王宁, 王树青. PID自适应调整增益的神经元非模型控制[J]. 机电工程, 1999, 5, 72- 73.
	ZHANG J M , WANG N , WANG S Q . A neuron model-free controller with the adaptive gain regulated by the PID algorithm[J]. Mechanical and Electrical Engineering, 1999, 5, 72- 73.
26	韦常柱, 琚啸哲, 何飞毅, 等. 运载火箭主动段自适应增广控制[J]. 宇航学报, 2019, 40 (8): 918- 927.
	WEI C Z , JU X Z , HE F Y . Ascent flight adaptive augmenting control for launch vehicles[J]. Journal of Astronautics, 2019, 40 (8): 918- 927.
27	ZHANG L, WEI C Z, JING L. Heavy lift launch vehicle technology of adaptive augmented fault tolerant control[C]//Proc. of the Chinese Guidance, Navigation and Control Conference, 2016.
28	崔乃刚, 陈诚, 潘哲, 等. 运载火箭自适应增广抗扰减载控制[J]. 导弹与航天运载技术, 2017, 6, 1- 6.
	CUI N G , CHEN C , PAN Z , et al. Adaptive augmented disturbance rejection and load-relief control for launch vehicle[J]. Missiles and Space Vehicles, 2017, 6, 1- 6.
29	何飞毅. 重型运载火箭模型参考自适应增广控制研究[D]. 哈尔滨: 哈尔滨工业大学, 2018.
	HE F Y. Research on model reference adaptive augmenting control of heavy lift launch vehicle[D]. Harbin: Harbin Institute of Technology, 2018.
30	徐世昊. 运载火箭自适应增广抗扰控制研究[D]. 哈尔滨: 哈尔滨工业大学, 2020.
	XU S H. Resaerch on adaptive augmenting disturbance rejection control for launch vehicle[D]. Harbin: Harbin Institute of Technology, 2020.
31	张晋. 固体运载器自适应增广抗扰姿态控制方法研究[D]. 哈尔滨: 哈尔滨工业大学, 2020.
	ZHANG J. Adaptive augmented disturbance rejection attitude control method for solid launch vehicle[D]. Harbin: Harbin Institute of Technology, 2020.
32	祝大利. 运载火箭传感器布局与自适应增广控制研究[D]. 大连: 大连理工大学, 2020.
	ZHU D L. Research on sensor layout and adaptive augmenting control of a launch vehicle[D]. Dalian: Dalian University of Technology, 2020.
33	DOMENICO T , ALESSANDRO Z , GUIDO D M . Optimal tuning of adaptive augmenting controller for launch vehicles in atmospheric flight[J]. Journal of Guidance, Control, and Dynamics, 2020, 43 (11): 2133- 2140.
34	TANNEN S V, MICHAEL R H, JOHN H W. Evaluating the stability of NASA's space launch system with adaptive augmenting control[C]//Proc. of the 10th International ESA Conference on Guidance, Navigation and Control Systems, 2017.
35	MARK J B, TANNEN S V, MICHAEL R H. Nonlinear(Lyapunov) stability of the space launch system flight control system with adaptive augmenting control[C]//Proc. of the AIAA Scitech Forum, 2019.
36	ANGELOV J, YOON Y E, JOHNSON E N, et al. Analytical derivation of the sinusoidal input describing function for adaptive augmenting control algorithms[C]//Proc. of the AIAA Guidance, Navigation, and Control Conference, 2018.

[1]	Yushi JIANG, Yang CHEN, Lu GAO, Ligen CAI, Jixing LYU. Predefined-time adaptive control for heavy-lift launch vehicles [J]. Systems Engineering and Electronics, 2023, 45(8): 2570-2577.
[2]	Xu CHEN, Yao XIAO, Lingyu YANG, Jing ZHANG. Stability analysis of radome parasitic loop based on simplified model [J]. Systems Engineering and Electronics, 2023, 45(6): 1784-1796.
[3]	Xinfeng WU, Qibo PENG, Ran HUANG, Jinglin LI. Escape and rescue strategy of launch vehicle ascending section based on MBSE [J]. Systems Engineering and Electronics, 2023, 45(4): 1121-1126.
[4]	Yanli DU, Wu LIU, Mingming TANG, Yuhui WANG. Robust predictor-corrector guidance with multiple constraints for reusable launch vehicles [J]. Systems Engineering and Electronics, 2021, 43(5): 1316-1325.
[5]	Shuai LIU, Guorong ZHAO, Bin ZENG, Chao GAO. Moving horizon estimation for uncertain systems with packet dropouts and quantization [J]. Systems Engineering and Electronics, 2020, 42(4): 912-918.
[6]	SUN Guoxin, XIA Qunli, ZHANG Daochi, XU Wenbo. Piecewise guidance strategy of auto landing for reusable launch vehicle [J]. Systems Engineering and Electronics, 2019, 41(4): 856-862.
[7]	LV Jian-wei, XIE Zong-ren, XU Yi-fan. Requirement’s determining and optimization on fault isolation’s ambiguity group size of weapon system [J]. Systems Engineering and Electronics, 2016, 38(5): 1208-.
[8]	HOU De-long, WANG Qing, DONG Chao-yang, HUANG Xi-yuan. Adaptive tracking control for switched polytopic system of hypersonic vehicle [J]. Systems Engineering and Electronics, 2014, 36(5): 926-933.
[9]	SHI Junyou， WANG Lu， LI Haiwei， WANG Fengwu. Quantitative analysis of system testability based on design characteristics [J]. Journal of Systems Engineering and Electronics, 2012, 34(2): 418-423.
[10]	FU Jian-ping, LU Min-yan, LIU Bin. Software testability analysis based on framework [J]. Journal of Systems Engineering and Electronics, 2011, 33(9): 2133-2138.
[11]	HE Cheng-long, CHEN Xin, YANG Yi-dong. Mixed programming control allocation for reusable launch vehicles using dynamic inverse calculating [J]. Journal of Systems Engineering and Electronics, 2010, 32(9): 1973-1976.
[12]	ZHANG Jun, HUANG Yi-ming, Yang Yi-dong. Research on 3-D guidance trajectory propagation of terminal area energy management for RLVs [J]. Journal of Systems Engineering and Electronics, 2010, 32(8): 1727-1731.
[13]	HE Cheng-long, CHEN Xin, YANG Yi-dong. Ascent trajectory design for reusable launch vehicles [J]. Journal of Systems Engineering and Electronics, 2010, 32(5): 1034-1037.
[14]	GUO Wen-cheng, SHI Wu-xi, GUO Li-jin. Adaptive fuzzy control for a class of uncertain nonlinear systems [J]. Journal of Systems Engineering and Electronics, 2010, 32(2): 351-354.
[15]	WANG Dong-mei,FANG Hua-jing. Research on swarm behavior in arbitrarily finite dimensional spaces [J]. Journal of Systems Engineering and Electronics, 2010, 32(11): 2447-2452.

Parameters design and stability margin analysis of adaptive augmenting control for launch vehicle

RichHTML

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

Figures/Tables 9

References 36

Related Articles 15

Recommended Articles

Metrics

Comments