变质心机构动态响应下的平流层飞艇纵向运动仿真

doi:10.1007/s12204-022-2552-0

J Shanghai Jiaotong Univ Sci ›› 2024, Vol. 29 ›› Issue (6): 1139-1150.doi: 10.1007/s12204-022-2552-0

变质心机构动态响应下的平流层飞艇纵向运动仿真

徐敏杰1,2，王全保1，段登平1

（1. 上海交通大学航空航天学院，上海200240；2. 西北核技术研究所，西安710024）

收稿日期:2021-10-08 接受日期:2021-11-19 出版日期:2024-11-28 发布日期:2024-11-28

Longitudinal Motion Simulation of Stratospheric Airship Under Dynamic Response of Moving-Mass Actuator

XU Minjie^1,2(徐敏杰), WANG Quanbao^1∗ (王全保), DUAN Dengping¹(段登平)

(1. School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China; 2. Northwest Institute of Nuclear Technology, Xi’an 710024, China）

Received:2021-10-08 Accepted:2021-11-19 Online:2024-11-28 Published:2024-11-28

摘要/Abstract

摘要： 提出了一种总质量恒定的平流层动质量飞艇的设计方法，并推导了基于牛顿-欧拉法的一般动力学方程。考虑滑块命令响应的时滞性以及与飞艇状态参数的动态耦合，设计了具有输入约束和状态约束的位置跟踪控制器，使得滑块动态响应系统具有临界阻尼特性。以动质量平流层飞艇的纵向姿态运动为研究对象，进行了参数化建模和姿态控制仿真，并分析了不同质量比下动质量控制的姿态控制能力。仿真结果表明：姿态控制能力不受气流速度的影响，滑块质量比是影响姿态控制能力的主要因素。滑块控制器的参数直接影响姿态控制的动态性能，也决定了飞艇的动态耦合水平。与基于气动控制面的姿态控制相比，动质量控制能使飞行器在稳态时的气流速度和攻角收敛到初始状态，并保持良好的气动外形。

关键词: 平流层飞艇, 滑块, 动态响应, 姿态控制

Abstract: In this paper, a design method of moving-mass stratospheric airship with constant total mass is presented, and the general dynamics equation based on Newton-Euler method is derived. Considering the timedelay of the slider command response and the dynamic coupling to the airship’s state parameters, a position tracking controller with input and state constraints was designed to make the dynamic response system of the slider have critical damping characteristics. By taking the longitudinal attitude motion of moving-mass stratospheric airship as the research object, parametric modeling and attitude control simulation were carried out, and the attitude control ability of moving-mass control under different mass ratios was analyzed. The simulation results show that the attitude control ability is not affected by airspeed, and the mass ratio of slider is the main factor affecting the attitude control ability. The parameters of the slider controller have a direct influence on the dynamic performance of attitude control and also determine the dynamic coupling level of the airship. Compared with the attitude control based on the aerodynamic control surface, moving-mass control can make the airspeed and attack angle converged to the initial state at the steady state, and keep a good aerodynamic shape.

中图分类号:

V249

徐敏杰1, 2, 王全保1, 段登平1. 变质心机构动态响应下的平流层飞艇纵向运动仿真[J]. J Shanghai Jiaotong Univ Sci, 2024, 29(6): 1139-1150.

XU Minjie^{1, 2}(徐敏杰), WANG Quanbao^1∗ (王全保), DUAN Dengping¹(段登平). Longitudinal Motion Simulation of Stratospheric Airship Under Dynamic Response of Moving-Mass Actuator[J]. J Shanghai Jiaotong Univ Sci, 2024, 29(6): 1139-1150.

参考文献

[1] HOU Z X, YANG X X, QIAO K, et al. Stratospheric airship technology [M]. Beijing: Science Press, 2019 (in Chinese).
[2] ONDA M, MORIKAWA Y. High-altitude lighter-than-air powered platform [R]. Warrendale: SAE Technical Paper, 1991: 687-694.
[3] COLOZZA A, DOLCE J. Initial feasibility assessment of a high altitude long endurance airship: NASA CR212724 [R]. Washington: NASA, 2003.
[4] CHU A, BLACKMORE M, OHOLENDT R, et al. A novel concept for stratospheric communications and surveillance: The StarLight [C]//AIAA Balloon Systems Conference. Williamsburg: AIAA, 2007: 2601.
[5] ZHENG W, YANG Y N, WU J. Survey of flight control for the stratosphere airship [J]. Flight Dynamics, 2013,31(3): 193-197 (in Chinese).
[6] REGAN F J, KAVETSKY R A. Add-on controller for ballistic reentry vehicles [J]. IEEE Transactions on Automatic Control, 1984, 12(6): 869-880.
[7] DENG Y G, BAO Y P, LEI J W, et al. Research on composite control of new air vehicle [J]. Acta Simulata Systematica Sinica, 2005, 17(7): 1531-1534 (in Chinese).
[8] GAO M W, SHAN X X. By changing position research of airship’s center of gravity to control longitudinal motion [J]. Chinese Quarterly of Mechanics. 2006, 27(4):714-728 (in Chinese).
[9] SMITH I, LEE M K, FORTNEBERRY M, et al. HiSentinel80: flight of a high altitude airship [C]//11th AIAA Aviation Technology, Integration, and Operations Conference. Virginia Beach: AIAA, 2011: 6973.
[10] LEE M, SMITH I, ANDROULAKAKIS S. Highaltitude LTA airship efforts at the US army SMDC/ARSTRAT [C]//18th AIAA Lighter-Than-Air Systems Technology Conference. Seattle: AIAA, 2009:2852.
[11] ZHOU G, CHEN L, DONG Q. Modeling and analysis of moving-mass actuated stratospheric airship [J]. High Technology Letters, 2013, 19(2): 145-149.
[12] WANG F, ZHOU J H, MIAO J G. Pitch handling characteristics of the stratospheric airship based on moving mass control [C]//2016 35th Chinese Control Conference. Chengdu: IEEE, 2016: 10915-10920.
[13] CHEN L, ZHOU G, YAN X J, et al. Composite control of stratospheric airships with moving masses [J].Journal of Aircraft, 2012, 49(3): 794-801.
[14] OUYANG J, QU W D, XI Y G. Stratospheric verifying airship modeling and analysis [J]. Journal of Shanghai Jiao Tong University, 2003, 37(6): 956-960 (in Chinese).
[15] YANG Y N. Dynamics modeling and flight control for a stratospheric airship [D]. Changsha: National University of Defense Technology, 2013 (in Chinese).
[16] MIAO J G. Dynamics analysis & motion control of airship [D]. Beijing: University of Chinese Academy of Sciences (Space Science and Applications Research Center), 2008 (in Chinese).
[17] MUELLER J, PALUSZEK M, ZHAO Y. Development of an aerodynamic model and control law design for a high altitude airship [C]//AIAA 3rd “Unmanned Unlimited” Technical Conference, Workshop and Exhibit.Chicago: AIAA, 2004: 6479.
[18] OUYANG J. Research on modeling and control of unmanned airship [D]. Shanghai: Shanghai Jiaotong University, 2003 (in Chinese).
[19] SCHMITENDORF W E, BARMISH B R. Null controllability of linear systems with constrained controls[J]. SIAM Journal on Control and Optimization, 1980,18(4): 327-345.

变质心机构动态响应下的平流层飞艇纵向运动仿真

Longitudinal Motion Simulation of Stratospheric Airship Under Dynamic Response of Moving-Mass Actuator

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