Abstract
This paper aims to mitigate the vulnerability of an aircraft to radar detection arising from inherent design limitations by proposing a technique to generate maneuvers that reduce the aircraft's radar cross-section (RCS) below a specified threshold when exposed to dynamic (mobile) radar threats. The proposed approach utilizes control barrier functions and exploits the relationship between control inputs and the RCS, with the required RCS database for the baseline aircraft generated through numerical analyzes. The outcomes are contrasted with a virtual path that omits RCS constraints and maintains the aircraft's rotational attitude stationary. Simulation results validate the effectiveness of the proposed methodology, as evidenced by a comparison with the virtual trajectory, where the RCS reaches up to 25 dBsm. In contrast, the CBF-pilot approach keeps the RCS at the predefined threshold of 0 dBsm throughout the maneuver.
| Original language | English |
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| Title of host publication | 2025 IEEE Conference on Control Technology and Applications, CCTA 2025 |
| Editors | Christopher Vermillion, Sorin Olaru, Johanna Mathieu, Mehmet Mercangoz, Stephanie Stockar, Alireza Karimi, Timm Faulwasser, Eric Kerrigan, Rolf Fineisen, Sebastien Gros, Ionela Prodan, Christopher Edwards, Fabrizio Dabbene, Airlie Chapman, Behrouz Touri |
| Publisher | Institute of Electrical and Electronics Engineers Inc. |
| Pages | 208-213 |
| Number of pages | 6 |
| ISBN (Electronic) | 9798331539085 |
| DOIs | |
| Publication status | Published - 2025 |
| Event | 9th IEEE Conference on Control Technology and Applications, CCTA 2025 - San Diego, United States Duration: 25 Aug 2025 → 27 Aug 2025 |
Publication series
| Name | 2025 IEEE Conference on Control Technology and Applications, CCTA 2025 |
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Conference
| Conference | 9th IEEE Conference on Control Technology and Applications, CCTA 2025 |
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| Country/Territory | United States |
| City | San Diego |
| Period | 25/08/25 → 27/08/25 |
Bibliographical note
Publisher Copyright:© 2025 IEEE.
Keywords
- control barrier functions
- low-observability
- maneuver generation
- radar cross-section
- survivability