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タイトルConceptual Design Optimization of an Augmented Stability Aircraft Incorporating Dynamic Response and Actuator Constraints
本文(外部サイト)http://hdl.handle.net/2060/20140011926
著者(英)Welstead, Jason; Crouse, Gilbert L., Jr.
発行日2014-01-13
言語eng
内容記述Empirical sizing guidelines such as tail volume coefficients have long been used in the early aircraft design phases for sizing stabilizers, resulting in conservatively stable aircraft. While successful, this results in increased empty weight, reduced performance, and greater procurement and operational cost relative to an aircraft with optimally sized surfaces. Including flight dynamics in the conceptual design process allows the design to move away from empirical methods while implementing modern control techniques. A challenge of flight dynamics and control is the numerous design variables, which are changing fluidly throughout the conceptual design process, required to evaluate the system response to some disturbance. This research focuses on addressing that challenge not by implementing higher order tools, such as computational fluid dynamics, but instead by linking the lower order tools typically used within the conceptual design process so each discipline feeds into the other. In thisresearch, flight dynamics and control was incorporated into the conceptual design process along with the traditional disciplines of vehicle sizing, weight estimation, aerodynamics, and performance. For the controller, a linear quadratic regulator structure with constant gains has been specified to reduce the user input. Coupling all the disciplines in the conceptual design phase allows the aircraft designer to explore larger design spaces where stabilizers are sized according to dynamic response constraints rather than historical static margin and volume coefficient guidelines.
NASA分類Aircraft Stability and Control; Aircraft Design, Testing and Performance; Fluid Mechanics and Thermodynamics
レポートNONF1676L-17983
AIAA Paper 2014-0187
権利Copyright, Distribution as joint owner in the copyright


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