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13.2: Flight Mechanics - Aircraft motion

  • Page ID
    78424
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    This exercise consists in obtaining and analyzing the 3DOF performances of a BADA model aircraft. The evolution of aircraft state variables over time \((V(t), \gamma (t), \chi (t), x_e(t), y_e(t), h_e(t), m(t))\), including the 4D trajectory \((x_e, y_e, h_e, t)\), in a typical flight of a commercial transportation aircraft are to be analysed. An aircraft type among those in BADA database (See [1]) will be chosen. Python programming Language will be used to integrate the resulting set of differential equations and plot the results.


    13.2: Flight Mechanics - Aircraft motion is shared under a CC BY-SA 3.0 license and was authored, remixed, and/or curated by Manuel Soler Arnedo via source content that was edited to conform to the style and standards of the LibreTexts platform; a detailed edit history is available upon request.

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