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An Online Trajectory Planning Method for Hypersonic Aircraft Considering Maneuverability

  • Bolun Gao
  • , Yidi Yao
  • , Hao Cheng
  • , Langfu Cui*
  • , Baijun Liu
  • , Chenggang Bai
  • *Corresponding author for this work
  • Beihang University

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

The hypersonic aircraft possesses high-speed flight capabilities but lacks maneuverability, making it challenging to simultaneously consider timeliness, optimality, and maneuver constraints in trajectory planning when faced with sudden threats. For this issue, this paper proposes an online trajectory planning algorithm that considers maneuverability - the Eccentric Tightening Trajectory Planning method. Upon the A∗ algorithm, this method generates a search grid based on obstacle edges to reduce search complexity and utilizes Dubins curves to ensure maneuver constraints. Through comparisons with classical A∗ and DWA algorithms in three scenarios, simulation results demonstrate that the proposed algorithm satisfies maneuverability constraints, meets the efficiency requirements of online planning, and exhibits higher efficiency in scenarios with longer distances and fewer threats.

Original languageEnglish
Title of host publication2024 4th International Conference on Computer, Control and Robotics, ICCCR 2024
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages323-327
Number of pages5
ISBN (Electronic)9798350373141
DOIs
StatePublished - 2024
Event4th International Conference on Computer, Control and Robotics, ICCCR 2024 - Shanghai, China
Duration: 19 Apr 202421 Apr 2024

Publication series

Name2024 4th International Conference on Computer, Control and Robotics, ICCCR 2024

Conference

Conference4th International Conference on Computer, Control and Robotics, ICCCR 2024
Country/TerritoryChina
CityShanghai
Period19/04/2421/04/24

Keywords

  • A
  • Dubins curve
  • algorithm
  • avoid obstacles
  • hypersonic vehicle
  • path planning

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