Piecewise Trajectory and Angle Constraint-Based Fractional-Order Sliding Mode Control

被引:4
作者
Fan, Junfang [1 ]
Chen, Shiwei [2 ]
Wang, Wei [2 ]
Ji, Yi [1 ]
Liu, Ning [1 ]
机构
[1] Beijing Informat Sci & Technol Univ, Beijing Key Lab High Dynam Nav Technol, Beijing 100192, Peoples R China
[2] Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
基金
中国国家自然科学基金;
关键词
Weapons; Trajectory; Sliding mode control; Laser modes; Aerodynamics; Calculus; Uncertainty; Fractional-order sliding-mode guidance law (FOSMGL); lag compensation; miniature munition; piecewise trajectory planning; GUIDANCE LAW; IMPACT TIME; MISSILES; DESIGN;
D O I
10.1109/TAES.2023.3281310
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This article proposes an approach for piecewise trajectory planning and fractional-order sliding-mode guidance of a two-stage launched miniature munition with the laser beam riding steered guidance technology. In the proposed approach, first, the polynomial description is used as an expected trajectory. Then consider the random external disturbances/parametric uncertainties and other factors deteriorate the tracking control performances of the miniature munition. To reduce the chattering caused by modeling errors and external disturbances and achieve fast speed and high-accuracy tracking performances for miniature munition, based on adaptive multipower reaching strategy, an integrated guidance and control (IGC) method with the fractional-order sliding-mode guidance law (FOSMGL) is introduced. The designed fractional-order sliding surfaces ultimately and successively allow both the trajectory and the attitude angle converge to expected value in a finite time. In addition, considering the case of a moving target, a feedforward compensation mechanism, which decreases the lag of the guidance system, is imposed using an additional compensated term obtained from the attitude angle error. The convergence and reachability of the proposed algorithm in finite-time are analyzed using the Lyapunov function method. The validity and practicability of the proposed method are verified by a numerical example.
引用
收藏
页码:6782 / 6797
页数:16
相关论文
共 31 条
[1]   Differential geometric guidance based on the involute of the target's trajectory [J].
Ariff, O ;
Zbikowski, R ;
Tsourdos, A ;
White, BA .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2005, 28 (05) :990-996
[2]   Finite-time stability of continuous autonomous systems [J].
Bhat, SP ;
Bernstein, DS .
SIAM JOURNAL ON CONTROL AND OPTIMIZATION, 2000, 38 (03) :751-766
[3]   Nonsingular Sliding Mode Guidance for Impact Time Control [J].
Cho, Dongsoo ;
Kim, H. Jin ;
Tahk, Min-Jea .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2016, 39 (01) :61-68
[4]   Three-Dimensional Nonlinear Differential Geometric Path-Following Guidance Law [J].
Cho, Namhoon ;
Kim, Youdan ;
Park, Sanghyuk .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2015, 38 (12) :2366-2385
[5]   Fractional terminal sliding mode control design for a class of dynamical systems with uncertainty [J].
Dadras, Sara ;
Momeni, Hamid Reza .
COMMUNICATIONS IN NONLINEAR SCIENCE AND NUMERICAL SIMULATION, 2012, 17 (01) :367-377
[6]   Adaptive fractional order control of doubly fed induction generator based wind energy conversion system under uncertainty [J].
Delavari, Hadi ;
Sharifi, Ali .
JOURNAL OF RENEWABLE AND SUSTAINABLE ENERGY, 2021, 13 (03)
[7]   Optimal In-Flight Trajectory Modifications for Ballistic Missiles and Free Rockets [J].
Druckmann, Erez ;
Ben-Asher, Joseph Z. .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2012, 35 (02) :462-470
[8]  
Esmaeilzadeh SM, 2021, INT J CONTROL AUTOM, V19, P767
[9]   A Multiple Power Reachable Sliding Mode Control Approach for Guidance of Miniature Laser Beam Riding Steered Munition [J].
Fan, Jun-Fang ;
Chen, Shi-Wei .
INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2021, 2021
[10]   SMC-Based Integrated Guidance and Control for Beam Riding Missiles With Limited LBPU [J].
Guo, Jianguo ;
Peng, Qian ;
Guo, Zongyi .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2021, 57 (05) :2969-2978