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时空约束条件下多旋翼机动轨迹优化方法

科研成果: 期刊稿件文章同行评审

摘要

Multicopter are often used in complex and variable scenarios such as post-earthquake search and rescue, geological exploration, etc. Considering their endurance and environmental characteristics, optimizing the flight trajectory of multicopter to complete tasks better and faster has become a key issue. To this end, a multicopter's traversing indoor diagonal slit mission is set up, and a trajectory optimization method under multi-constraint based on the parabolic principle and the Pontryagin's minimum principle is proposed. By imitating the process of throwing things through a narrow window and from the perspective of analyzing the oblique slit of the task object, a parabolic trajectory is designed to guide the aircraft to cross the oblique slit with inertia. For the initial state required to throw the aircraft, Pontryagin's minimum principle is usedto realize the state transition trajectory. A 3D model was built in MATLAB to verify the crossing effect. The experiment shows that the multicopter can pass through the inclined seam with a vertical tilt of 63° or a horizontal tilt of 32°.

投稿的翻译标题Maneuver trajectory optimization method of multicopter under space-time constraints
源语言繁体中文
页(从-至)231-239
页数9
期刊Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
47
2
DOI
出版状态已出版 - 2月 2021

关键词

  • Multi-constraint
  • Multicopter
  • Parabolic principle
  • State transition
  • Trajectory optimization

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