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- W2107764241 abstract "This paper presents a unified rational function approximation (RFA) formulation to take into account the influence of aeroelastic effects on the flight dynamic behavior of the whole aircraft. Standard production flutter engineering models that incorporate translational and rotational rigid-body degrees of freedom are usually not able to recover the traditional flight dynamic equations of motion due to several inherent conflicting modeling objectives. This paper identifies key elements within the RFA to update the unsteady aerodynamic model. By allowing the inclusion of gravity-related terms, vertical acceleration related stability derivatives, as well as lift and drag forces due to forward velocity perturbations into the RFA matrices, it is shown by closed-form solutions that the usual flight dynamic equations of motion are fully recovered. In this way, open and closed-loop simulations of the aeroelastic/aeroservoelastic response of the whole aircraft would be available to the flight control engineer to design and validate dependable flight control systems. Its implementation will naturally extend the RFA setup into a flight dynamic oriented class. To illustrate the modeling framework, the proposed technique is demonstrated using two examples: i) Navion, and ii) Predator B “Hunter Killer” aircrafts." @default.
- W2107764241 created "2016-06-24" @default.
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- W2107764241 date "2006-05-01" @default.
- W2107764241 modified "2023-09-25" @default.
- W2107764241 title "Unified Rational Function Approximation Formulation for Aeroelastic and Flight Dynamics Analyses" @default.
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- W2107764241 doi "https://doi.org/10.2514/6.2006-2025" @default.
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