UAV formations control using high order sliding modes

被引:41
作者
Galzi, D. [1 ]
Shtessel, Y. [2 ]
机构
[1] Univ Alabama, Dept Elect & Comp Engn, Huntsville, AL 35899 USA
[2] Univ Alabama, Huntsville, AL 35899 USA
来源
2006 AMERICAN CONTROL CONFERENCE, VOLS 1-12 | 2006年 / 1-12卷
关键词
D O I
10.1109/ACC.2006.1657386
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Formations of Unmanned Aerial Vehicles' (UAV) using High/Second Order Sliding Mode (HOSM/SOSM) controllers are studied. The purpose of the study is to control the formation of several agents, or a swarm of UAVs, using robust and continuous controllers to achieve leader/followers collision-free path-tracking formation in the presence of unknown bounded disturbances acting on each UAV. A strategic formation expansion process is developed allowing extensive formation of n agents through a chain of predefined strategies. Computer simulations of three, four, and six UAVs demonstrate a collision-free flight formation while continuing on a specific path. All formations remain in the presence of unknown bounded disturbances via bounded, robust, accurate and continuous SOSM controls, specifically applying Super-twist control method.
引用
收藏
页码:4249 / 4254
页数:6
相关论文
共 14 条
[1]  
Chen Q, 2003, 42ND IEEE CONFERENCE ON DECISION AND CONTROL, VOLS 1-6, PROCEEDINGS, P516
[2]  
Edwards C., 1998, Sliding Mode Control: Theory and Applications
[3]   Dynamic and control issues of formation flight [J].
Giulietti, F ;
Innocenti, M ;
Napolitano, M ;
Pollini, L .
AEROSPACE SCIENCE AND TECHNOLOGY, 2005, 9 (01) :65-71
[4]  
Isidori A, 1995, NONLINEAR CONTROL SYSTEMS DESIGN 1995, VOLS 1 AND 2, P87
[5]  
Justh E., 2003, P 42 IEEE C DEC CONT
[6]   Robust exact differentiation via sliding mode technique [J].
Levant, A .
AUTOMATICA, 1998, 34 (03) :379-384
[7]   Universal single-input-single-output (SISO) sliding-mode controllers with finite-time convergence [J].
Levant, A .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2001, 46 (09) :1447-1451
[8]  
PACHTER M, 1999, AIAA GUID NAV CONTR
[9]  
PROUD WW, 1999, P 1999 AIAA GUID NAV
[10]  
SHKOLNIKOV IA, 2001, P 2001 C GUID NAV CO