![]() Natural Frequency (NatFreq) Download NatFreq.m As shown, there are twelve original state elements, four longitudinal controls, three lateral-directional controls, and three disturbances. It presents matrices for body or hybrid/stability axes, for longitudinal or lateral-directional partitions, and for fourth- or sixth-order computations. It either passes the matrices unchanged, re-orders elements of the matrices, or generates a selected reduced-order model from them. LonLatDir.m accepts stability and control-effect matrices for longitudinal and lateral-directional dynamics. Supporting Functions Reduced-Order Models (LonLatDir) Download LonLatDir.m Examples of FmodelFile.mat, GmodelFile.mat, and ControlData.mat are included. The chosen model is summarized in ControlData.mat. The nominal trimmed flight condition also is stored in FmodelFile.mat. ![]() SURVEY.m makes calculations based on the (12 x 12) Fmodel, (12 x 7) Gmodel, and (12 x 3) Lmodel matrices that are stored in FmodelFile.mat and GmodelFile.mat by FLIGHTv2.m.
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