AIAA Modeling and Simulation Technologies Conference 2015
DOI: 10.2514/6.2015-2036
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Effective Model size for the prediction of the lateral control envelope of damaged aircraft

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“…Controls consisted of a right-hand sidestick with pitch trim control, rudder pedals with force feedback, and thrust, flap, and gear levers. A nonlinear aerodynamic model was used from a light twin-propeller aircraft: the Piper PA-34 Seneca III ( De Muynck & Hesse, 1990 ; Koolstra, Herman, & Mulder, 2015 ). The aircraft model has certain properties and failure options, which allows for the development of challenging flying tasks.…”
Section: Methodsmentioning
confidence: 99%
“…Controls consisted of a right-hand sidestick with pitch trim control, rudder pedals with force feedback, and thrust, flap, and gear levers. A nonlinear aerodynamic model was used from a light twin-propeller aircraft: the Piper PA-34 Seneca III ( De Muynck & Hesse, 1990 ; Koolstra, Herman, & Mulder, 2015 ). The aircraft model has certain properties and failure options, which allows for the development of challenging flying tasks.…”
Section: Methodsmentioning
confidence: 99%