Robust Nonlinear Disturbance Observer Based Adaptive Guidance Law Against Uncertainties in Missile Dynamics and Target Maneuver

被引:53
作者
Chwa, Dongkyoung [1 ]
机构
[1] Ajou Univ, Dept Elect & Comp Engn, Suwon 443749, South Korea
基金
新加坡国家研究基金会;
关键词
2ND-ORDER SLIDING MODES; CONTROL LOOP DYNAMICS; HOMING MISSILE; ACCELERATION; DESIGN;
D O I
10.1109/TAES.2018.2801392
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The proposed robust nonlinear disturbance observer based adaptive guidance method considers the nonlinear coupled missile dynamics and rapidly maneuvering target. It also includes unavailable information such as high-order line-of-siglit rates and target acceleration as time-varying parametric uncertainties and nonparametric disturbances. An integrated guidance and control model, a robust nonlinear disturbance observer, a nonlinear missile jerk observer, and a robust nonlinear guidance law are proposed, the validity of which is demonstrated by stability analysis and simulations.
引用
收藏
页码:1739 / 1749
页数:11
相关论文
共 31 条
[1]  
[Anonymous], 1995, NONLINEAR ADAPTIVE C
[2]   Target Maneuver Adaptive Guidance Law for a Bounded Acceleration Missile [J].
Atir, Ronen ;
Hexner, Gyorgy ;
Weiss, Haim ;
Shima, Tal .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2010, 33 (03) :695-706
[3]   GUIDANCE OF A HOMING MISSILE VIA NONLINEAR GEOMETRIC CONTROL METHODS [J].
BEZICK, S ;
RUSNAK, I ;
GRAY, WS .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1995, 18 (03) :441-448
[4]   Homing missile guidance and estimation under agile target acceleration [J].
Chen, Robert H. ;
Speyert, Jason L. ;
Lianos, Dimitrios .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2007, 30 (06) :1577-1589
[5]   Fast Adaptive Guidance Against Highly Maneuvering Targets [J].
Cho, Dongsoo ;
Kim, H. Jin ;
Tahk, Min-Jea .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2016, 52 (02) :671-680
[6]  
Choi JY, 2006, IEEE T AERO ELEC SYS, V42, P659, DOI 10.1109/TAES.2006.1642580
[7]   Observer-based adaptive guidance law considering target uncertainties and control loop dynamics [J].
Chwa, D ;
Choi, JY ;
Anavatti, SG .
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2006, 14 (01) :112-123
[8]   Adaptive nonlinear guidance law considering control loop dynamics [J].
Chwa, D ;
Choi, JY .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2003, 39 (04) :1134-1143
[9]   New parametric affine modeling and control for skid-to-turn missiles [J].
Chwa, D ;
Choi, JY .
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2001, 9 (02) :335-347
[10]  
Chwa D., 2004, IEEE TRANSACTIONS ON, V12, P335