Earticle

초록

영어

With the extensive use of UAV, how to make the UAV avoid the obstacle and arrive at the destination has become a hot issue. To make the angle shift minimum, a method on dynamic guidance obstacle avoidance of UAV based on the minimum angle shift is proposed, considering the constraints such as the completion time of obstacle, the motor performance, the direction of velocity after obstacle avoidance and so on, determining the range of guidance parameters. In the meanwhile, the obstacle method is extended to 3D-space based on 2D. Moreover, numerical simulations are carried out to verify the effectiveness of the method.

목차

Abstract
 1. Introduction
 2. The Judgment of Collision and the Establishment of Kinematics Equations
  2.1 Collision Judgment
  2.2 The Establishment of Kinematics Equations
 3. The Obstacle Avoidance Guidance Strategy based on the Minimum Angle Shift
  3.1 The Design of Obstacle Avoidance Guidance Law based on the Minimum Angle Shift
  3.2 Stability Proof
  3.3 Velocity Solution of UAV
  3.4 Simulation Analysis
 4. Study on 3D Obstacle Avoidance
  4.1 Study on Dimensionality Reduction Obstacle Avoidance
  4.2 The Simulation Analysis
 5. Conclusion
 Acknowledgements
 References

키워드

저자

• Xiong zhiyong [ Science and Technology on Avionics Integration Laboratory, Shanghai, China ]
• Yang Xiuxia [ Department of Control Engineering, Naval Aeronautical and Astronautical University, Yantai, China ]
• Zhang Yi [ Department of Control Engineering, Naval Aeronautical and Astronautical University, Yantai, China ]
• Hua Wei [ Department of Control Engineering, Naval Aeronautical and Astronautical University, Yantai, China ]
• Liu Xiaowei [ Department of Control Engineering, Naval Aeronautical and Astronautical University, Yantai, China ]

참고문헌

발행기관

간행물

표지보기 관심저널 등록

• 간행물명

  International Journal of Security and Its Applications

• 간기

  격월간

• pISSN

  1738-9976

• 수록기간

  2008~2016

• 등재여부

  SCOPUS

• 십진분류

  KDC 505 DDC 605