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  4. Design and synthesis of a hierarchical hybrid controller for quadrotor navigation
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Design and synthesis of a hierarchical hybrid controller for quadrotor navigation

Full metadata

Description

There has been exciting progress in the area of Unmanned Aerial Vehicles (UAV) in the last decade, especially for quadrotors due to their nature of easy manipulation and simple structure. A lot of research has been done on achieving autonomous and robust control for quadrotors. Recently researchers have been utilizing linear temporal logic as mission specification language for robot motion planning due to its expressiveness and scalability. Several algorithms have been proposed to achieve autonomous temporal logic planning. Also, several frameworks are designed to compose those discrete planners and continuous controllers to make sure the actual trajectory also satisfies the mission specification. However, most of these works use first-order kinematic models which are not accurate when quadrotors fly at high speed and cannot fully utilize the potential of quadrotors.

This thesis work describes a new design for a hierarchical hybrid controller that is based on a dynamic model and seeks to achieve better performance in terms of speed and accuracy compared with some previous works. Furthermore, the proposed hierarchical controller is making progress towards guaranteed satisfaction of mission specification expressed in Linear Temporal Logic for dynamic systems. An event-driven receding horizon planner is also utilized that aims at distributed and decentralized planning for large-scale navigation scenarios. The benefits of this approach will be demonstrated using simulations results.

Date Created
2016
Contributors
  • Zhang, Xiaotong (Author)
  • Fainekos, Georgios (Thesis advisor)
  • Ben Amor, Heni (Committee member)
  • Shrivastava, Aviral (Committee member)
  • Arizona State University (Publisher)
Topical Subject
  • Computer Engineering
  • Cyber-Physical Systems
  • Hybrid Controller
  • Quadrotor
  • PID controllers
  • Drone aircraft--Automatic control.
  • Drone aircraft
Resource Type
Text
Genre
Masters Thesis
Academic theses
Extent
ix, 68 pages : illustrations (some color)
Language
eng
Copyright Statement
In Copyright
Reuse Permissions
All Rights Reserved
Primary Member of
ASU Electronic Theses and Dissertations
Peer-reviewed
No
Open Access
No
Handle
https://hdl.handle.net/2286/R.I.37036
Statement of Responsibility
by Xiaotong Zhang
Description Source
Viewed on April 22, 2016
Level of coding
full
Note
Partial requirement for: M.S., Arizona State University, 2016
Note type
thesis
Includes bibliographical references (pages 61-63)
Note type
bibliography
Field of study: Computer science
System Created
  • 2016-04-01 08:00:26
System Modified
  • 2021-08-30 01:25:10
  •     
  • 1 year 8 months ago
Additional Formats
  • OAI Dublin Core
  • MODS XML

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