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      SCIE SCOPUS KCI등재

      Lateral Vehicle Control Based on Active Flight Control Technology

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      다국어 초록 (Multilingual Abstract)

      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.
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      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 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.

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      목차 (Table of Contents)

      • 영어 초록
      • 1. Introduction
      • 2. CCV Mode for an Advanced Aircraft
      • 3. Lateral Vehicle Dynamics with Four Wheel
      • 4. Formulations of CCV Mode Control
      • 영어 초록
      • 1. Introduction
      • 2. CCV Mode for an Advanced Aircraft
      • 3. Lateral Vehicle Dynamics with Four Wheel
      • 4. Formulations of CCV Mode Control
      • 5. Simulations and Results
      • 6. Concluding Remark
      • Acknowledgments
      • References
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