Lateral vehicle control based on active flight control technology

被引:0
作者
Seo, Young Bong
Choi, Jae Weon [1 ]
Guang Ren Duan
机构
[1] Pusan Natl Univ, Sch Mech Engn, Pusan 609735, South Korea
[2] Pusan Natl Univ, Res Inst Mech Technol, Pusan 609735, South Korea
[3] Harbin Inst Technol, Ctr Control Theory & Guidance Technol, Harbin 150001, Peoples R China
关键词
active control technology (ACT); control configured vehicle (CCV); flight control system; lateral vehicle control; 4WS; eigenstructure assignment; command generator tracker; motion decoupling; multi-variable control;
D O I
10.1007/BF02915997
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In this paper, a lateral vehicle control using the concept of control configured vehicle (CCV) is presented. The control objectives for the lateral dynamics of a vehicle include the ability to follow a chosen variable without significant motion change in other specified variables. The analysis techniques for decoupling of the aircraft motions are utilized to develop vehicle lateral control with advanced mode. Vehicle lateral dynamic is determined to have the steering input and control torque input. The additional vehicle modes are also defined to using CCV concept. We use right eigenstructure assignment techniques and command generator tracker to design a control law for an lateral vehicle dynamics. The desired eigenvectors are chosen to achieve the desired decoupling (i.e., lateral direction speed and yaw rate). The command generator tracker is used to ensure steady-state tracking of the driver's command. Finally, the developed design is utilized by using the lateral vehicle dynamic with four wheel.
引用
收藏
页码:981 / 992
页数:12
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