Title :
Lateral Vehicle Control Using the CCV Mode Control
Author :
Young Bong Seo ; Jae Weon Choi ; Guang Ren Duan
Author_Institution :
Sch. of Mech. Eng., Pusan Nat. Univ., South Korea
Abstract :
In this paper, 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 late). 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 wheels.
Keywords :
aircraft control; control system analysis; control system synthesis; eigenstructure assignment; motion control; multivariable control systems; CCV mode control; active control technology; aircraft motion decoupling; command generator tracker; control analysis; control configured vehicle; control law design; control torque input; driver command; eigenstructure assignment; eigenvectors; flight control system; lateral direction speed; multivariable control; steady-state tracking; steering; vehicle lateral control; vehicle lateral dynamics; yaw late; Aerospace control; Aircraft; Control systems; Motion control; Stability; Steady-state; Tires; Torque control; Vehicle dynamics; Wheels; 4WS; Active Control Technology(ACT); Command Generator Tracker; Control Configured Vehicle(CCV); Eigenstructure Assignment; Flight Control System; Lateral Vehicle Control; Motion Decoupling; Multi-variable Control;
Conference_Titel :
Control Conference, 2006. CCC 2006. Chinese
Conference_Location :
Harbin
Print_ISBN :
7-81077-802-1
DOI :
10.1109/CHICC.2006.280584