This paper discusses a computationally efficient algorithm for estimating the safe maneuvering envelope of damaged aircraft. The algorithm performs a robust reachability analysis through an optimal control formulation while making use of time scale separation and taking into account uncertainties in the aerodynamic derivatives. This approach differs from others since it is physically inspired. This more transparent approach allows interpreting data in each step, and it is assumed that these physical models based upon flight dynamics theory will therefore facilitate certification for future real life applications.
Safe Maneuvering Envelope Estimation Based on a Physical Approach
AIAA Guidance, Navigation, and Control Conference 2013 ; 2013 ; Boston, MA, United States
2013-08-18
Conference paper
No indication
English
Safe Maneuvering Envelope Estimation based on a Physical Approach (AIAA 2013-4618)
British Library Conference Proceedings | 2013
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