Date of Award

Spring 6-13-2025

Document Type

Dissertation

Degree Name

Ph.D. in Electrical Engineering

Organizational Unit

Daniel Felix Ritchie School of Engineering and Computer Science, Electrical and Computer Engineering

First Advisor

Kimon P. Valavanis

Second Advisor

Matthew J. Rutherford

Third Advisor

Patrizia Liveri

Fourth Advisor

Alvaro Arias

Fifth Advisor

Rui Fan

Sixth Advisor

Michael J. Keables

Copyright Statement / License for Reuse

All Rights Reserved
All Rights Reserved.

Keywords

Hexacopters, Autonomous navigation, Autonomy, Control, Mars, Reinforcement learning, Space exploration

Abstract

Mars exploration has recently witnessed major interest within the scientific community. Unmanned robotic platforms offer reliable solutions to acquire and collect data and information from the Red Planet. Particularly, rovers, landers, and orbiters have significantly shaped planetary exploration on the Moon and Mars, contributing significantly to past missions while also highlighting limitations in their capacity to cover diverse terrains over wide ranges. Given current advances in Unmanned Aircraft Systems (UASs), Unmanned Aerial Vehicles (UAVs) offer promising alternatives for future scientific missions.

It is argued that hexacopters, with their relatively compact design and redundancy, present a promising solution for autonomous exploration tasks on Mars, overcoming at the same time the limitations of wheel-based rovers and increasing orbiters’ data resolution. However, the specific harsh conditions of the Martian environment result in a restricted flight envelope when flying close to the surface and then landing. To this end, autonomous navigation strategies along with robust controllers are needed for complex exploration tasks.

This research focuses on designing a Mars Hexacopter (MHex) for a scouting mission in the Martian Jezero region. The hexacopter configuration and architecture considers, as a initial baseline, the NASA conceptual study of the Mars Science Helicopter (MSH). Then, the mission profile for mapping the Belva crater is examined, followed by a detailed approach to implement and test autonomous observer-based navigation and control strategies. A comprehensive simulated environment is also presented based on integrating ROS and Ardupilot, which is used to validate the overall system architecture and the mission parameters considering both the morphological shape of the explored crater and the atmospheric conditions of Mars.

Copyright Date

6-2025

Publication Statement

Copyright is held by the author. User is responsible for all copyright compliance.

Rights Holder

Laura Sopegno

Provenance

Received from ProQuest

File Format

application/pdf

Language

English (eng)

Extent

115 pgs

File Size

8.7 MB



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