Abstract
In this paper, a novel guidance scheme is presented for UAVs using the Integrated Guidance and Control (IGC) framework. The proposed guidance scheme is derived using H∞ Loop Shaping Design Procedure (LSDP). To recover from an initial cross track error, the proposed guidance algorithm produces such aileron commands that ensure the roll maneuvers without saturating the roll angle. The shaping of the open loop plant is carried out using the pre and post weights and then the robust stabilization is done by using the normalized left coprime factor uncertainty. The performance and robustness of the system are verified by introducing parametric uncertainties in to the system model. The results of the proposed scheme are verified by implementing it on a complete 6-DOF nonlinear model in the presence of wind disturbance. The simulation results indicate the effectiveness and robustness of the proposed guidance algorithm.
| Original language | English |
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| Title of host publication | 2015 20th International Conference on Methods and Models in Automation and Robotics, MMAR 2015 |
| Publisher | Institute of Electrical and Electronics Engineers Inc. |
| Pages | 523-528 |
| Number of pages | 6 |
| ISBN (Electronic) | 9781479987016 |
| DOIs | |
| State | Published - 29 Sep 2015 |
| Externally published | Yes |
| Event | 20th International Conference on Methods and Models in Automation and Robotics, MMAR 2015 - Miedzyzdroje, Poland Duration: 24 Aug 2015 → 27 Aug 2015 |
Publication series
| Name | 2015 20th International Conference on Methods and Models in Automation and Robotics, MMAR 2015 |
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Conference
| Conference | 20th International Conference on Methods and Models in Automation and Robotics, MMAR 2015 |
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| Country/Territory | Poland |
| City | Miedzyzdroje |
| Period | 24/08/15 → 27/08/15 |
Bibliographical note
Publisher Copyright:© 2015 IEEE.
ASJC Scopus subject areas
- Artificial Intelligence
- Computer Vision and Pattern Recognition
- Control and Systems Engineering