Research on Three-Dimensional Integrated Guidance and Control Design with Multiple Constraints

被引:3
作者
Fu, Zhenhua [1 ]
Zhang, Kuanqiao [2 ]
Yang, Suochang [3 ]
机构
[1] Beijing Inst Technol, Sch Automat, Beijing, Peoples R China
[2] State Key Lab Complex Electromagnet Environm Effe, Luoyang, Peoples R China
[3] Army Engn Univ, Shijiazhuang, Hebei, Peoples R China
关键词
SLIDING MODE CONTROL; IMPACT ANGLE; MISSILE;
D O I
10.1155/2022/6296770
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this paper, a fixed-time convergence-integrated guidance and control (IGC) method is proposed, which considers terminal line-of-sight (LOS) angle constraint, full-state constraints, and input saturation. Firstly, an IGC design model considering the full coupling of three channels is constructed, and a fixed-time convergence disturbance observer is used to estimate and compensate the unknown disturbances in the model. Secondly, based on the fixed-time stability theory, sliding mode control, and backstepping control, a novel IGC scheme is carried out, and the second-order instruction filter is used to restrict the system states and control instructions. Furthermore, the fixed-time stability of the close-loop system is proved and the expression of convergence time upper bound is given. Finally, comparison simulation and Monte Carlo simulation verify the effectiveness and superiority of the proposed IGC algorithm.
引用
收藏
页数:18
相关论文
共 26 条
[1]   Multivariable continuous fixed-time second-order sliding mode control: design and convergence time estimation [J].
Basin, Michael ;
Panathula, Chandrasekhara Bharath ;
Shtessel, Yuri .
IET CONTROL THEORY AND APPLICATIONS, 2017, 11 (08) :1104-1111
[2]   Finite-time integrated guidance and control system for hypersonic vehicles [J].
Chong Zhenyu ;
Guo Jianguo ;
Zhao Bin ;
Guo Zongyi ;
Lu Xiaodong .
TRANSACTIONS OF THE INSTITUTE OF MEASUREMENT AND CONTROL, 2021, 43 (04) :842-853
[3]   Guidance and control with fixed-time convergence for an interception missile [J].
Cui, Lei ;
Jin, Nan ;
Zong, Yantao .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2022, 236 (09) :1705-1720
[4]   Integrated Guidance and Control with Input Saturation and Impact Angle Constraint [J].
Fu, Zhenhua ;
Zhang, Kuanqiao ;
Gan, Qintao ;
Yang, Suochang .
DISCRETE DYNAMICS IN NATURE AND SOCIETY, 2020, 2020
[5]   Three-dimensional multivariable integrated guidance and control design for maneuvering targets interception [J].
He, Shaoming ;
Wang, Wei ;
Wang, Jiang .
JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2016, 353 (16) :4330-4350
[6]   Continuous second-order sliding mode based impact angle guidance law [J].
He, Shaoming ;
Lin, Defu ;
Wang, Jiang .
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 41 :199-208
[7]   Fixed-Time Attitude Control for Rigid Spacecraft With Actuator Saturation and Faults [J].
Jiang, Boyan ;
Hu, Qinglei ;
Friswell, Michael I. .
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2016, 24 (05) :1892-1898
[8]   Robust extended state observer-based three dimensional integrated guidance and control design for interceptors with impact angle and input saturation constraints [J].
Khankalantary, Saeed ;
Sheikholeslam, Farid .
ISA TRANSACTIONS, 2020, 104 :299-309
[9]   Integrated guidance and control with partial state constraints and actuator faults [J].
Liu, Wangkui ;
Wei, Yiyin ;
Hou, Mingzhe ;
Duan, Guangren .
JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2019, 356 (09) :4785-4810
[10]   Robust design approach of three-dimensional integrated guidance and control containing impact angle constraints [J].
Liu X.-D. ;
Huang W.-W. ;
Du L.-F. .
Kongzhi Lilun Yu Yingyong/Control Theory and Applications, 2016, 33 (11) :1535-1542