Design of the horizontal oppression of light aircraft

According to the results of the general design of the light six-seat whole-composite aircraft, the following work was performed by me: a constructive-power scheme of horizontal oppression (GO) was developed; the optimum geometric dimensions and parameters of the GO and its aggregates were calculated and selected; the model of the distribution of the internal space of the GO and its aggregates was created; the design calculation of the elements of the structure of the GO was performed; the elements of the structure of the GO and its aggregates were modeled, the elements of the control system of the GO.