Investigating Flight Envelope Variation Predictability of Impaired Aircraft using Least-Squares Regression Analysis
Ramin Norouzi, Amirreza Kosari, Mohammad Hossein Sabour

TL;DR
This study explores the predictability of flight envelope changes in impaired aircraft using linear and nonlinear least-squares models, aiming to enhance in-flight safety by anticipating control loss due to failures.
Contribution
It introduces polynomial and hyperbolic tangent models to predict flight envelope variations, providing a novel approach to assess aircraft failure impacts.
Findings
Models predict envelope variation with good accuracy
Polynomial models enable sensitivity analysis of failure parameters
Hyperbolic tangent models effectively capture nonlinear envelope changes
Abstract
Aircraft failures alter the aircraft dynamics and cause maneuvering flight envelope to change. Such envelope variations are nonlinear and generally unpredictable by the pilot as they are governed by the aircraft's complex dynamics. Hence, in order to prevent in-flight Loss of Control it is crucial to practically predict the impaired aircraft's flight envelope variation due to any a-priori unknown failure degree. This paper investigates the predictability of the number of trim points within the maneuvering flight envelope and its centroid using both linear and nonlinear least-squares estimation methods. To do so, various polynomial models and nonlinear models based on hyperbolic tangent function are developed and compared which incorporate the influencing factors on the envelope variations as the inputs and estimate the centroid and the number of trim points of the maneuvering flight…
Peer Reviews
No public reviews on file for this paper yet. If you reviewed it on a platform where reviews are public (OpenReview, ICLR, NeurIPS, ICML), you can paste yours below so the community can read it here.
Videos
No videos yet. Explain this paper in a talk, walkthrough, or lecture? Add one.
