Please use this identifier to cite or link to this item: https://scholarbank.nus.edu.sg/handle/10635/80556
Title: Identifying aerial bomb's aerodynamic drag coefficient curve using optimal dynamic fitting method
Authors: Chen, Yangquan 
Wen, Changyun
Sun, Mingxuan 
Issue Date: Nov-1998
Citation: Chen, Yangquan,Wen, Changyun,Sun, Mingxuan (1998-11). Identifying aerial bomb's aerodynamic drag coefficient curve using optimal dynamic fitting method. Journal of Aircraft 35 (6) : 971-975. ScholarBank@NUS Repository.
Abstract: The aerodynamic curve identification of aerial bomb from three-degree-of-freedom positional measurements is formulated as an optimal tracking control problem (OTCP). By using a spline parameterization of the drag coefficient curve that is taken as the control profile, the OTCP is converted into a parametric minimization problem where the proposed quasi-Newton-Raphson iteration is used to cut the computational cost. The inaccurate initial states can be corrected easily.
Source Title: Journal of Aircraft
URI: http://scholarbank.nus.edu.sg/handle/10635/80556
ISSN: 00218669
Appears in Collections:Staff Publications

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