论文

基于INDI的倾转旋翼无人机过渡模式控制方案

  • 刘双喜 ,
  • 林泽淮 ,
  • 刘伟 ,
  • 闫斌斌 ,
  • 黄伟
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  • 1.国防科技大学 空天科学学院,长沙 410073
    2.国防科技大学 高超声速技术实验室,长沙 410073
    3.西北工业大学 航天学院,西安 710072
    4.上海航天设备制造总厂有限公司,上海 200245
.E-mail: gladrain2001@163.com

收稿日期: 2023-10-08

  修回日期: 2023-12-20

  录用日期: 2024-02-07

  网络出版日期: 2024-02-23

基金资助

湖南省杰出青年基金(2021JJ10045);西北工业大学硕士研究生实践创新能力培育基金(PF2023046)

Transition mode control scheme of tilt rotor UAV based on INDI

  • Shuangxi LIU ,
  • Zehuai LIN ,
  • Wei LIU ,
  • Binbin YAN ,
  • Wei HUANG
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  • 1.College of Aerospace Science and Engineering,National University of Defense Technology,Changsha  410073,China
    2.Hypersonic Technology Laboratory,National University of Defense Technology,Changsha  410073,China
    3.School of Astronautics,Northwestern Polytechnical University,Xi’an  710072,China
    4.Shanghai Aerospace Equipment Manufacturer Co. ,Ltd,Shanghai  200245,China

Received date: 2023-10-08

  Revised date: 2023-12-20

  Accepted date: 2024-02-07

  Online published: 2024-02-23

Supported by

Natural Science Foundation of Hunan Province of China(2021JJ10045);The Practice and Innovation Funds for Graduate Students of Northwestern Polytechnical University(PF2023046)

摘要

针对倾转旋翼无人机(TRUAV)过渡模式控制问题,提出了一种基于增量非线性动态逆(INDI)的控制方案。首先,基于四轴倾转旋翼无人机动力学特性,建立了面向控制的纵向运动模型;随后,研究了虚拟控制量与控制量分配方法,在此基础上设计了倾转旋翼无人机过渡模式自适应倾转方案;然后,基于增量非线性动态逆控制理论,分别设计了高度、速度和姿态回路过渡模式下内/外环控制器,以及旋翼和舵面控制量混合策略。最后,仿真实验验证了基于虚拟控制量分配的自适应倾转方案的有效性,以及高度、速度和姿态回路控制器的鲁棒性。

本文引用格式

刘双喜 , 林泽淮 , 刘伟 , 闫斌斌 , 黄伟 . 基于INDI的倾转旋翼无人机过渡模式控制方案[J]. 航空学报, 2024 , 45(17) : 529685 -529685 . DOI: 10.7527/S1000-6893.2024.29685

Abstract

This paper proposes an Incremental Nonlinear Dynamic Inverse (INDI) control scheme for the problem of transition mode control of Tilt Rotor Unmanned Aerial Vehicle (TRUAV). Firstly, based on the dynamic characteristics of the quadrotor TRUAV, a longitudinal motion model suitable for control is established. Then, the virtual control command and control allocation methods are studied, and an adaptive tilt scheme for the transition mode of the TRUAV is designed based on these methods. Subsequently, based on the incremental nonlinear dynamic inverse control theory, the inner/outer loop controllers for the altitude, velocity and attitude transition modes are designed, as well as a mixed control method for rotor and rudder deflection control quantities. Finally, simulation experiments validate the effectiveness of the adaptive tilt scheme based on virtual control command allocation, as well as the robustness of the altitude, velocity, and attitude controllers.

参考文献

1 刘佳豪, 李高华, 王福新. 倾转过渡状态旋翼-机翼气动干扰特性[J]. 航空学报202243(12): 126097.
  LIU J H, LI G H, WANG F X. Rotor-wing aerodynamic interference characteristics in conversion mode[J]. Acta Aeronautica et Astronautica Sinica202243(12): 126097 (in Chinese).
2 LIU Z, HE Y Q, YANG L Y, et al. Control techniques of tilt rotor unmanned aerial vehicle systems: A review[J]. Chinese Journal of Aeronautics201730(1): 135-148.
3 DING C W, LU L. A tilting-rotor unmanned aerial vehicle for enhanced aerial locomotion and manipulation capabilities: design, control, and applications[J]. IEEE/ASME Transactions on Mechatronics202126(4): 2237-2248.
4 LIU Z, THEILLIOL D, HE Y Q, et al. Active model-based nonlinear system identification of quad tilt-rotor UAV with flight experiments[J]. Science China Information Sciences202265(8): 182202.
5 CARDOSO D N, ESTEBAN S, RAFFO G V. A new robust adaptive mixing control for trajectory tracking with improved forward flight of a tilt-rotor UAV[J]. ISA Transactions2021110: 86-104.
6 SHENG H L, ZHANG C, XIANG Y L. Mathematical modeling and stability analysis of tiltrotor aircraft[J]. Drones20226(4): 92.
7 左卓. 无人倾转旋翼机过渡段纵向控制策略研究[D]. 南京: 南京航空航天大学, 2020.
  ZUO Z. Research on longitudinal control strategy of unmanned tilting rotor conversion mode[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2020 (in Chinese).
8 陈在斌. 倾转旋翼无人机控制系统关键技术研究[D]. 长春:中国科学院长春光学精密机械与物理研究所, 2020.
  CHEN Z B. Research on key technologies of flight control system of A tilt rotor UAV[D].Changchun: Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, 2020 (in Chinese).
9 LI S M, LV Z Y, FENG L, et al. Nonlinear cascade control for a new coaxial tilt-rotor UAV[J]. International Journal of Control, Automation and Systems202220(9): 2948-2958.
10 ALLENSPACH M, DUCARD G J J. Model predictive control of a convertible tiltrotor unmanned aerial vehicle[C]∥2020 28th Mediterranean Conference on Control and Automation (MED). Piscataway: IEEE Press, 2020: 715-720.
11 韩丽敏. 倾转旋翼机过渡段纵向控制技术研究[D]. 南京: 南京航空航天大学, 2011.
  HAN L M. Research on longitudinal control technology of tiltrotor aircraft in transition flight phase[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2011 (in Chinese).
12 刘海波. 菱形翼布局倾转旋翼无人机滑模非线性飞行控制研究[D]. 西安: 西北工业大学, 2019.
  LIU H B. Research on sliding mode nonlinear flight control for diamond wing tilt rotor UAV[D]. Xi’an: Northwestern Polytechnical University, 2019 (in Chinese).
13 凡永华, 杨军, 赖水清, 等. 倾转旋翼机过渡段最优飞行控制系统设计[J]. 飞行力学200725(1): 47-50.
  FAN Y H, YANG J, LAI S Q, et al. Design of an optimal flight control system for tiltrotor conversion[J]. Flight Dynamics200725(1): 47-50 (in Chinese).
14 陈嘉先, 梁波. 倾转旋翼无人机模态转换控制[J]. 战术导弹技术2015(2): 70-76.
  CHEN J X, LIANG B. Control of tilt rotor unmanned aerial vehicle during mode transition[J]. Tactical Missile Technology2015(2): 70-76 (in Chinese).
15 严旭飞, 陈仁良. 倾转旋翼机动态倾转过渡过程的操纵策略优化[J]. 航空学报201738(7): 520865.
  YAN X F, CHEN R L. Control strategy optimization of dynamic conversion procedure of tilt-rotor aircraft[J]. Acta Aeronautica et Astronautica Sinica201738(7): 520865 (in Chinese).
16 肖斯奇, 余帆, 施啸宇. 倾转旋翼无人机过渡段纵向控制策略设计研究[J]. 导航定位与授时20218(6): 88-95.
  XIAO S Q, YU F, SHI X Y. Research on longitudinal control strategy design in transition section of tilt-rotor UAV[J]. Navigation Positioning and Timing20218(6): 88-95 (in Chinese).
17 刘安, 余宗金, 廖保全, 等. 四旋翼式飞行潜航器非线性增量动态逆控制[J]. 飞行力学202240(2): 67-73.
  LIU A, YU Z J, LIAO B Q, et al. Incremental nonlinear dynamic inversion control for a quad-rotor aerial underwater vehicle[J]. Flight Dynamics202240(2): 67-73 (in Chinese).
18 STEFFENSEN R, STEINERT A, SMEUR E J J. Nonlinear dynamic inversion with actuator dynamics: an incremental control perspective[J]. Journal of Guidance, Control, and Dynamics202246(4): 709-717.
19 LIU Z, ZHANG Y, LIANG J J, et al. Application of the improved incremental nonlinear dynamic inversion in fixed-wing UAV flight tests[J]. Journal of Aerospace Engineering202235(6): 04022091.
20 AHMADI K, ASADI D, NABAVI-CHASHMI S Y, et al. Modified adaptive discrete-time incremental nonlinear dynamic inversion control for quad-rotors in the presence of motor faults[J]. Mechanical Systems and Signal Processing2023188: 109989.
21 翟友鸿, 李春涛, 苏子康 等. 基于神经网络增量动态逆的高速靶机筋斗机动控制[J/OL]. 北京航空航天大学学报,(2024-01-12) [2024-01-16]. .
  ZHAI Y H, LI C T, SU Z K, et al. Neural network incremental dynamic inversion target drone somersault maneuver control[J/OL]. Journal of Beijing University of Aeronautics and Astronautics, (2024-01-12) [2024-01-16]. (in Chinese).
22 LI Y, LIU X X, LU P, et al. Angular acceleration estimation-based incremental nonlinear dynamic inversion for robust flight control[J]. Control Engineering Practice2021117: 104938.
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