2012 | OriginalPaper | Buchkapitel
Engineering Modeling and Simulation for New Estimation of Aircraft’s Dynamic Angles
verfasst von : Zhao Wu, Lixin Wang
Erschienen in: System Simulation and Scientific Computing
Verlag: Springer Berlin Heidelberg
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The measurement of aircraft’s dynamic angles is difficult and inaccurate due to the precarious flight environment. This paper brings forward and amends a new estimation of aircraft’s angle of attack and sideslip angle based on the basic of INS/GPS data. Through engineering modeling of closed-loop flight simulation framework and estimation method, the result shows obvious rationality and veracity.