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- W2488934178 abstract "The derivation and linearization of equations of motion for spinning vehicles is presented in this paper. Two reference frames are used for the basis of the derivations. The non-rotating body frame and the rotating body frame are used to establish state-space representations. An eigenvalue and eigenvector analysis presents the modes of flight for each reference frame using an asymmetrical body. The non-rotating body frame equations of motion results in five roots; three stable real poles and two identical complex conjugate pairs. This frame is found to be useful for control and linearised simulation of axisymmetrical vehicles, where the control mechanism can be decoupled from the spinning body. This frame is not useful for modelling an asymmetrical spinning vehicle. The analysis of the rotating body frame equations results in six non-zero roots; three real, stable poles, two different complex conjugate pairs and a marginally unstable real pole. Two of the real poles are dependant on the reference roll angle chosen for the analysis. It was found that the rotating body frame is appropriate for controller design, where the controller input is a requested angle of attack, sideslip angle, pitch rate or yaw rate. It is not applicable to a controller with a requested pitch or yaw angle." @default.
- W2488934178 created "2016-08-23" @default.
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- W2488934178 date "2009-06-14" @default.
- W2488934178 modified "2023-09-26" @default.
- W2488934178 title "Comparison of Reference Frames in the Linearization of Flight Dynamics for Spinning Vehicles" @default.
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- W2488934178 doi "https://doi.org/10.2514/6.2009-5841" @default.
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