Abstract
Vehicle impairment is one of the primary contributing factors that lead to Loss of Control. Preventing such events requires a comprehensive understanding of the aircraft behaviour under the impaired conditions. Performance and stability aspects of the impaired aircraft are normally addressed individually in previous studies. Constrained bifurcation analysis and continuation has been used in this paper, with the advantage that both performance and stability can be assessed simultaneously. Moreover, the results provide insight into the analysis of safe landing capability and the effectiveness of initiatives aimed at enhancing survivability. A modified numerical procedure is outlined and computational examples of a large transport aircraft under impaired condition are presented.
Original language | English |
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Title of host publication | AIAA SciTech 2018 |
Subtitle of host publication | 2018 AIAA Atmospheric Flight Mechanics Conference, paper no. AIAA 2018-0775 |
Publisher | American Institute of Aeronautics and Astronautics Inc. (AIAA) |
ISBN (Print) | 9781624105258 |
Publication status | Published - 7 Jan 2018 |
Event | AIAA Atmospheric Flight Mechanics Conference, 2018 - Kissimmee, United States Duration: 8 Jan 2018 → 12 Jan 2018 |
Conference
Conference | AIAA Atmospheric Flight Mechanics Conference, 2018 |
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Country/Territory | United States |
City | Kissimmee |
Period | 8/01/18 → 12/01/18 |