Control allocation in overactuated aircraft under position and rate limiting

被引:48
作者
Boskovic, JD [1 ]
Mehra, RK [1 ]
机构
[1] Sci Syst Co Inc, Woburn, MA 01801 USA
来源
PROCEEDINGS OF THE 2002 AMERICAN CONTROL CONFERENCE, VOLS 1-6 | 2002年 / 1-6卷
关键词
D O I
10.1109/ACC.2002.1024911
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Existing approaches to control allocation in overactuated aircraft under control input saturation are conservative. This is due to the fact that the solution to the corresponding constrained optimization problem may not be attainable with a chosen control input weighting matrix. On the other hand, there may exist a weighting matrix for which a solution exists under control input constraints. In this paper we propose two Control Allocation Algorithms (CAA) that can be used either on-line or off-line, and that, under an assumption that at least one solution to the tracking,control. design exists, finds that solution. The properties of the proposed CAAs are illustrated through simulations of the F/A-18C/D aircraft.
引用
收藏
页码:791 / 796
页数:6
相关论文
共 6 条
[1]   Adaptive control of a class of nonlinearly parameterized plants [J].
Boskovic, JD .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1998, 43 (07) :930-934
[2]  
BOSKOVIC JD, 2000, DESIGN ASSISTANT SOF
[3]  
BRINKER J, 1998, P 1998 AIAA GNC BOST
[4]  
ENNS D, 2000, P 1998 AIAA GNC BOST
[5]  
Narendra K., 1988, STABLE ADAPTIVE SYST
[6]  
PAGE A, 2000, P 2000 AIAA GNC DENV