Electronics and Electrical Engineering and Control

Tanker/UAV formation tracking control with hose connection constraints

  • Bo LIU ,
  • Zhongjie MENG
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  • 1.School of Astronautics,Northwestern Polytechnical University,Xi’an 710072,China
    2.National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University,Xi’an 710072,China

Received date: 2022-11-01

  Revised date: 2022-12-03

  Accepted date: 2022-12-29

  Online published: 2023-01-12

Supported by

National Natural Science Foundation of China(62173273);Natural Science Basic Research Plan in Shaanxi Province of China(2020JC-19)

Abstract

In autonomous aerial refueling mission, a leader-follower strategy based refueling formation flight control method is proposed for the formation flight problem under hose constraint after the docking of receiving Unmanned Aerial Vehicle(UAV) and the tanker. Firstly, a kinematic/dynamic model of the refueling formation under hose constraint is established. Then, a non-singular terminal sliding mode fast convergence controller is designed to meet the fast convergence requirements of refueling formation under hose constraint. For considering complex airflow disturbances and unknown hose disturbances, a trajectory tracking controller for UAV is designed by combining the extended state observer and PI type dynamic inversion control, and prove that the closed-loop system can achieve fast stabilization in finite time based on Lyapunov stability analysis. Finally, the effectiveness of the designed refueling formation tracking control method is verified by numerical simulation.

Cite this article

Bo LIU , Zhongjie MENG . Tanker/UAV formation tracking control with hose connection constraints[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023 , 44(17) : 328210 -328210 . DOI: 10.7527/S1000-6893.2022.28210

References

1 DARVISHPOOR S, ROSHANIAN J, RAISSI A, et al. Configurations, flight mechanisms, and applications of unmanned aerial systems: A review[J]. Progress in Aerospace Sciences2020121: 100694.
2 全权, 魏子博, 高俊, 等. 软管式自主空中加油对接阶段中的建模与控制综述[J]. 航空学报201435(9): 2390-2410.
  QUAN Q, WEI Z B, GAO J, et al. A survey on modeling and control problems for probe and drogue autonomous aerial refueling at docking stage[J]. Acta Aeronautica et Astronautica Sinica201435(9): 2390-2410 (in Chinese).
3 陆宇平, 杨朝星, 刘洋洋. 空中加油系统的建模与控制技术综述[J]. 航空学报201435(9): 2375-2389.
  LU Y P, YANG C X, LIU Y Y. A survey of modeling and control technologies for aerial refueling system[J]. Acta Aeronautica et Astronautica Sinica201435(9): 2375-2389 (in Chinese).
4 VALASEK J, KIMMETT J, HUGHES D, et al. Vision based sensor and navigation system for autonomous aerial refueling: AIAA-2002-3441[R]. Reston: AIAA, 2002.
5 TANDALE M D, BOWERS R, VALASEK J. Trajectory tracking controller for vision-based probe and drogue autonomous aerial refueling[J]. Journal of Guidance, Control, and Dynamics200629(4): 846-857.
6 WANG J, PATEL V V, CAO C Y, et al. Novel L1 adaptive control methodology for aerial refueling with guaranteed transient performance[J]. Journal of Guidance, Control, and Dynamics200831(1): 182-193.
7 WU J Z, LUO H D, AI J L. Docking controller for autonomous aerial refueling with adaptive dynamic surface control[J]. IEEE Access20208: 99846-99857.
8 SU Z K, WANG H L, YAO P, et al. Back-stepping based anti-disturbance flight controller with preview methodology for autonomous aerial refueling[J]. Aerospace Science and Technology201761: 95-108.
9 REN J R, DAI X H, QUAN Q, et al. Reliable docking control scheme for probe-drogue refueling[J]. Journal of Guidance, Control, and Dynamics201942(11): 2511-2520.
10 费伦, 段海滨, 徐小斌, 等. 基于变权重变异鸽群优化的无人机空中加油自抗扰控制器设计[J]. 航空学报202041(1): 323490.
  FEI L, DUAN H B, XU X B, et al. ADRC controller design for UAV based on variable weighted mutant pigeon inspired optimization[J]. Acta Aeronautica et Astronautica Sinica202041(1): 323490 (in Chinese).
11 吴慈航, 闫建国, 钱先云, 等. 受油机指定时间姿态稳定控制[J]. 航空学报202243(2): 324996.
  WU C H, YAN J G, QIAN X Y, et al. Predefined-time attitude stabilization control of receiver aircraft[J]. Acta Aeronautica et Astronautica Sinica202243(2): 324996 (in Chinese).
12 张国斌, 张青斌, 丰志伟, 等. 软式空中加油对接约束力不确定性分析[J]. 航空学报202142(9): 224517.
  ZHANG G B, ZHANG Q B, FENG Z W, et al. Uncertainty analysis on binding force of hose-drogue aerial refueling[J]. Acta Aeronautica et Astronautica Sinica202142(9): 224517 (in Chinese).
13 王海涛, 董新民, 郭军, 等. 空中加油软管锥套组合体甩鞭现象动力学建模与分析[J]. 航空学报201536(9): 3116-3127.
  WANG H T, DONG X M, GUO J, et al. Dynamics modeling and analysis of hose whipping phenomenon of aerial refueling hose-drogue assembly[J]. Acta Aeronautica et Astronautica Sinica201536(9): 3116-3127 (in Chinese).
14 DAI X H, WEI Z B, QUAN Q, et al. Hose-drum-unit modeling and control for probe-and-drogue autonomous aerial refueling[J]. IEEE Transactions on Aerospace and Electronic Systems202056(4): 2779-2791.
15 杜一江. 航空拖曳诱饵系统机动过程缆绳张力仿真[J]. 航空学报202142(9): 224495.
  DU Y J. Simulation on cable tension of aerial towed decoy system during maneuvers[J]. Acta Aeronautica et Astronautica Sinica202142(9): 224495 (in Chinese).
16 马东立, 刘亚枫, 林鹏. 航空拖曳诱饵系统的动态特性研究[J]. 航空学报201435(1): 161-170.
  MA D L, LIU Y F, LIN P. Study of dynamic characteristics of aeronautic towed decoy system[J]. Acta Aeronautica et Astronautica Sinica201435(1): 161-170 (in Chinese).
17 SUN L, BEARD R W. Towed-body trajectory tracking in aerial recovery of micro air vehicle in the presence of wind[C]∥Proceedings of the 2011 American Control Conference. Piscataway: IEEE Press, 2011: 3209-3214.
18 SU Z K, LI C T, ZHEN Z Y. Anti-disturbance constrained control of the air recovery carrier via an integral barrier Lyapunov function[J]. Aerospace Science and Technology2020106: 106157.
19 NICHOLS J W, SUN L, BEARD R W, et al. Aerial rendezvous of small unmanned aircraft using a passive towed cable system[J]. Journal of Guidance, Control, and Dynamics201437(4): 1131-1142.
20 SONG M S, HUANG P F. Dynamics and anti-disturbance control for tethered aircraft system[J]. Nonlinear Dynamics2022110(3): 2383-2399.
21 苏子康, 陈海通, 李春涛, 等. 非匹配包线下无人机空基回收拖曳系统协调运动规划[J]. 航空学报202344(10): 327377.
  Su Z K, CHEN H T, LI C T,et al. Coordinating motion planning for the towed cable system in UAV aerial recovery with unmatched envelope[J]. Acta Aeronautica et Astronautica Sinica202344(10): 327377 (in Chinese).
22 RO K, KUK T, KAMMAN J W. Dynamics and control of hose-drogue refueling systems during coupling[J]. Journal of Guidance, Control, and Dynamics201134(6): 1694-1708.
23 RO K, KAMMAN J W. Modeling and simulation of hose-paradrogue aerial refueling systems[J]. Journal of Guidance, Control, and Dynamics201033(1): 53-63.
24 PADHI R, RAKESH P. Formation flying of UAVs with dynamic inversion based partial integrated guidance and control: AIAA-2011-6600[R]. Portland. AIAA. 2011.
25 VO A T, KANG H J. An adaptive terminal sliding mode control for robot manipulators with non-singular terminal sliding surface variables[J]. IEEE Access20187: 8701-8712.
26 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: 183-242.
  HAN J Q. Active disturbance rejection control technique: The technique for estimating and compensating the uncertainties[M]. Beijing: National Defense Industry Press, 2008: 183-242 (in Chinese).
27 CHEN H, HE K F, QIAN W Q. Attitude control of UAV based on PI dynamic inversion[C]∥2016 35th Chinese Control Conference (CCC). Piscataway: IEEE Press, 2016: 10668-10672.
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