Dynamics and Control of a Multi-Rotor Aircraft
Despite the fact that aerodynamic loads (forces and moments) induced by airflow relative to a quadrotor vertical take-off and landing aircraft consist of both deterministic and stochastic components, all existing works on controlling the aircraft either ignore these loads or treat them as determini...
| Main Author: | |
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| Format: | Thesis |
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Curtin University
2016
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| Online Access: | http://hdl.handle.net/20.500.11937/54059 |
| _version_ | 1848759295203606528 |
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| author | Kava, Sean Anthony |
| author_facet | Kava, Sean Anthony |
| author_sort | Kava, Sean Anthony |
| building | Curtin Institutional Repository |
| collection | Online Access |
| description | Despite the fact that aerodynamic loads (forces and moments) induced by airflow relative to a quadrotor vertical take-off and landing aircraft consist of both deterministic and stochastic components, all existing works on controlling the aircraft either ignore these loads or treat them as deterministic. This simplification deteriorates the control performance in a practical implementation. This thesis presents a constructive design of controllers for a quadrotor aircraft to track a reference path in three-dimensional space under both deterministic and stochastic aerodynamic loads. |
| first_indexed | 2025-11-14T09:57:36Z |
| format | Thesis |
| id | curtin-20.500.11937-54059 |
| institution | Curtin University Malaysia |
| institution_category | Local University |
| last_indexed | 2025-11-14T09:57:36Z |
| publishDate | 2016 |
| publisher | Curtin University |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | curtin-20.500.11937-540592017-08-03T07:55:40Z Dynamics and Control of a Multi-Rotor Aircraft Kava, Sean Anthony Despite the fact that aerodynamic loads (forces and moments) induced by airflow relative to a quadrotor vertical take-off and landing aircraft consist of both deterministic and stochastic components, all existing works on controlling the aircraft either ignore these loads or treat them as deterministic. This simplification deteriorates the control performance in a practical implementation. This thesis presents a constructive design of controllers for a quadrotor aircraft to track a reference path in three-dimensional space under both deterministic and stochastic aerodynamic loads. 2016 Thesis http://hdl.handle.net/20.500.11937/54059 Curtin University fulltext |
| spellingShingle | Kava, Sean Anthony Dynamics and Control of a Multi-Rotor Aircraft |
| title | Dynamics and Control of a Multi-Rotor Aircraft |
| title_full | Dynamics and Control of a Multi-Rotor Aircraft |
| title_fullStr | Dynamics and Control of a Multi-Rotor Aircraft |
| title_full_unstemmed | Dynamics and Control of a Multi-Rotor Aircraft |
| title_short | Dynamics and Control of a Multi-Rotor Aircraft |
| title_sort | dynamics and control of a multi-rotor aircraft |
| url | http://hdl.handle.net/20.500.11937/54059 |